Explore: Shock Wave Interaction
Discover books, insights, and more — all in one place.
Learn more about Shock Wave Interaction with top reads curated from trusted sources — all in one place.
AI-Generated Overview About “shock-wave-interaction”:
Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1Numerical simulation of shock/turbulent boundary layer interaction
By Sedat Biringen
“Numerical simulation of shock/turbulent boundary layer interaction” Metadata:
- Title: ➤ Numerical simulation of shock/turbulent boundary layer interaction
- Author: Sedat Biringen
- Language: English
- Publisher: ➤ Dept. of Aerospace Engineering Sciences, University of Colorado - National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1993
- Publish Location: ➤ [Washington, D.C - Boulder, Colo - Springfield, Va
“Numerical simulation of shock/turbulent boundary layer interaction” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Turbulent flow - Turbulent boundary layer - Three dimensional models - Computerized simulation - Compressible boundary layer - Finite difference theory - Compressibility effects - Shock wave interaction - Energy transfer - Compressible flow - Nonlinear equations - Navier-Stokes equation - Supersonic flow - Shock waves
Edition Identifiers:
- The Open Library ID: OL17792155M - OL17684090M - OL18081888M
- Online Computer Library Center (OCLC) ID: 33958147
Access and General Info:
- First Year Published: 1993
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Numerical simulation of shock/turbulent boundary layer interaction at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
23-D Navier-Stokes analysis of crossing, glancing shocks/turbulent boundary layer interactions
By D. R. Reddy
“3-D Navier-Stokes analysis of crossing, glancing shocks/turbulent boundary layer interactions” Metadata:
- Title: ➤ 3-D Navier-Stokes analysis of crossing, glancing shocks/turbulent boundary layer interactions
- Author: D. R. Reddy
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1991
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“3-D Navier-Stokes analysis of crossing, glancing shocks/turbulent boundary layer interactions” Subjects and Themes:
- Subjects: ➤ Applications programs (Computers) - Hypersonic inlets - Navier-Stokes equation - Shock wave interaction - Three dimensional flow - Turbulent boundary layer - Viscous flow
Edition Identifiers:
- The Open Library ID: OL18072918M - OL17113112M - OL15399183M
Access and General Info:
- First Year Published: 1991
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find 3-D Navier-Stokes analysis of crossing, glancing shocks/turbulent boundary layer interactions at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
3Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction
By David S. Dolling
“Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction” Metadata:
- Title: ➤ Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction
- Author: David S. Dolling
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - Center for Aerodynamics Research, Dept. of Aerospace Engineering & Engineering Mechanics, University of Texas at Austin - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - Austin, Tex - [Washington, DC
“Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction” Subjects and Themes:
- Subjects: ➤ Turbulent boundary layer - Unsteady flow - Boundary layer separation - Aerodynamic loads - Corner flow - Vortex generators - Hypersonic boundary layer - Boundary layer control - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL18088579M - OL17803977M - OL15425915M
- Online Computer Library Center (OCLC) ID: 35454133
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
4An investigation of bleed configurations and their effect on shock wave/boundary layer interactions
By A. Hamed
“An investigation of bleed configurations and their effect on shock wave/boundary layer interactions” Metadata:
- Title: ➤ An investigation of bleed configurations and their effect on shock wave/boundary layer interactions
- Author: A. Hamed
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - University of Cincinnati - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Cincinnati, Ohio?] - [Washington, DC
“An investigation of bleed configurations and their effect on shock wave/boundary layer interactions” Subjects and Themes:
- Subjects: ➤ Corner flow - Engine design - Engine inlets - Oblique shock waves - Secondary flow - Separated flow - Shock wave interaction - Supersonic inlets
Edition Identifiers:
- The Open Library ID: OL15418954M - OL17793974M
- Online Computer Library Center (OCLC) ID: 34562841
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find An investigation of bleed configurations and their effect on shock wave/boundary layer interactions at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
5Flow characteristics in boundary layer bleed slots with plenum
By A. Hamed
“Flow characteristics in boundary layer bleed slots with plenum” Metadata:
- Title: ➤ Flow characteristics in boundary layer bleed slots with plenum
- Author: A. Hamed
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - For sale by the National Technical Information Service
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Washington, D.C
“Flow characteristics in boundary layer bleed slots with plenum” Subjects and Themes:
- Subjects: ➤ Boundary layer control - Boundary layer flow - Flow characteristics - Oblique shock waves - Plenum chambers - Pressure gradients - Shock wave interaction - Slots - Supersonic flow - Turbulent boundary layer
Edition Identifiers:
- The Open Library ID: OL17793989M - OL15419025M
- Online Computer Library Center (OCLC) ID: 34757915
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Flow characteristics in boundary layer bleed slots with plenum at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
6A time-accurate adaptive grid method and the numerical simulation of shock-vortex interaction
By Michael J. Bockelie
“A time-accurate adaptive grid method and the numerical simulation of shock-vortex interaction” Metadata:
- Title: ➤ A time-accurate adaptive grid method and the numerical simulation of shock-vortex interaction
- Author: Michael J. Bockelie
- Language: English
- Number of Pages: Median: 17
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - For sale by the National Technical Information Service
- Publish Date: 1990
- Publish Location: ➤ [Washington, D.C.] - Springfield, Va
“A time-accurate adaptive grid method and the numerical simulation of shock-vortex interaction” Subjects and Themes:
- Subjects: ➤ Grid generation (Mathematics) - Computerized simulation - Computational grids - Vortices - Shock wave interaction - Numerical grid generation (Numerical analysis)
Edition Identifiers:
- The Open Library ID: OL18257137M - OL16135232M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find A time-accurate adaptive grid method and the numerical simulation of shock-vortex interaction at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
7Simulation of January 1-7, 1978 events
By J. K. Chao
“Simulation of January 1-7, 1978 events” Metadata:
- Title: ➤ Simulation of January 1-7, 1978 events
- Author: J. K. Chao
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1987
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Simulation of January 1-7, 1978 events” Subjects and Themes:
- Subjects: ➤ Interplanetary space - Solar wind - Solar flares - Shock waves - Solar activity effects - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL18079890M - OL15411330M
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Simulation of January 1-7, 1978 events at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
8Mach 10 experimental database of a three-dimensional scramjet inlet flow field
By Scott D. Holland
“Mach 10 experimental database of a three-dimensional scramjet inlet flow field” Metadata:
- Title: ➤ Mach 10 experimental database of a three-dimensional scramjet inlet flow field
- Author: Scott D. Holland
- Language: English
- Number of Pages: Median: 214
- Publisher: ➤ Available from the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1995
- Publish Location: ➤ Hampton, Va - [Springfield, VA - Springfield, VA
“Mach 10 experimental database of a three-dimensional scramjet inlet flow field” Subjects and Themes:
- Subjects: ➤ Aerodynamics, Hypersonic - Air intakes - Airplanes - Computational fluid dynamics - Engine inlets - Flow distribution - Hypersonic Aerodynamics - Hypersonic speed - Inlet flow - Internal flow - Laminar boundary layer - Oblique shock waves - Pressure measurement - Ramjet engines - Scramjet engines - Shock wave interaction - Supersonic combustion ramjet engines - Three dimensional flow - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL16125691M - OL17141237M
- Online Computer Library Center (OCLC) ID: 33230284
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Mach 10 experimental database of a three-dimensional scramjet inlet flow field at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
9Blockage development in a transonic, axial compressor rotor
By Kenneth L. Suder
“Blockage development in a transonic, axial compressor rotor” Metadata:
- Title: ➤ Blockage development in a transonic, axial compressor rotor
- Author: Kenneth L. Suder
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1997
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“Blockage development in a transonic, axial compressor rotor” Subjects and Themes:
- Subjects: ➤ Laser anemometers - Blocking - Transonic flow - Flow characteristics - Shock wave interaction - Transonic compressors - Compressor rotors
Edition Identifiers:
- The Open Library ID: OL17837103M - OL15498505M
- Online Computer Library Center (OCLC) ID: 39821073
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Blockage development in a transonic, axial compressor rotor at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
10Experimental and computational investigation of the tip clearance flow in a transonic axial compressor rotor
By Kenneth L. Suder
“Experimental and computational investigation of the tip clearance flow in a transonic axial compressor rotor” Metadata:
- Title: ➤ Experimental and computational investigation of the tip clearance flow in a transonic axial compressor rotor
- Author: Kenneth L. Suder
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Experimental and computational investigation of the tip clearance flow in a transonic axial compressor rotor” Subjects and Themes:
- Subjects: ➤ Air speed - Airspeed - Applications programs (Computers) - Blade tips - Blade-vortex interaction - Compressor rotors - Laser anemometers - Shock wave interaction - Tip speed - Transonic compressors - Turbo compressors - Turbocompressors - Vortices - Wall flow
Edition Identifiers:
- The Open Library ID: OL17791893M - OL15414396M
- Online Computer Library Center (OCLC) ID: 34041388
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Experimental and computational investigation of the tip clearance flow in a transonic axial compressor rotor at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
113D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
By M. Mizukami
“3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet” Metadata:
- Title: ➤ 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
- Author: M. Mizukami
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Boundary layers - Supersonic diffusers - Computational grids - Boundary layer separation - Turbulence models - Three dimensional flow - Flow distribution - Engine inlets - Internal flow - Leading edges - Shock wave interaction - Navier-Stokes equation - Shock waves
Edition Identifiers:
- The Open Library ID: OL17117540M - OL17106503M
- Online Computer Library Center (OCLC) ID: 35282961
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
12Hypersonic flows as related to the national aerospace plane
By Marvin Kussoy
“Hypersonic flows as related to the national aerospace plane” Metadata:
- Title: ➤ Hypersonic flows as related to the national aerospace plane
- Author: Marvin Kussoy
- Language: English
- Number of Pages: Median: 57
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - Eloret Institute - For sale by the National Technical Information Service
- Publish Date: 1991 - 1995
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif - Sunnyvale, Calif
“Hypersonic flows as related to the national aerospace plane” Subjects and Themes:
- Subjects: ➤ Hypersonic flow - Aerospace planes - Computational fluid dynamics - Boundary layers - Flow measurement - Turbulence models - Flow distribution - Hypersonic speed - Wind tunnel tests - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL15419808M - OL19243299M
Access and General Info:
- First Year Published: 1991
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Hypersonic flows as related to the national aerospace plane at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
13Motion of the heliospheric termination shock
By Kamcilla Naidu
“Motion of the heliospheric termination shock” Metadata:
- Title: ➤ Motion of the heliospheric termination shock
- Author: Kamcilla Naidu
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Motion of the heliospheric termination shock” Subjects and Themes:
- Subjects: ➤ Interplanetary gas - Sun - Elastic waves - Shock waves - Heliosphere - Wave propagation - Shock discontinuity - Solar planetary interactions - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL15423311M - OL17796399M
- Online Computer Library Center (OCLC) ID: 35214123
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Motion of the heliospheric termination shock at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
14Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code
By Kamlesh Kapoor
“Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code” Metadata:
- Title: ➤ Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code
- Author: Kamlesh Kapoor
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Inlet flow - Two dimensional flow - Corner flow - Hypersonic inlets - Turbulent boundary layer - Hypersonic speed - Supersonic speed - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL15409264M - OL17788471M
- Online Computer Library Center (OCLC) ID: 32731299
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
15Validation of the RPLUS3D code for supersonic inlet applications involving three-dimensional shock wave boundary layer interactions
By Kamlesh Kapoor
“Validation of the RPLUS3D code for supersonic inlet applications involving three-dimensional shock wave boundary layer interactions” Metadata:
- Title: ➤ Validation of the RPLUS3D code for supersonic inlet applications involving three-dimensional shock wave boundary layer interactions
- Author: Kamlesh Kapoor
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Validation of the RPLUS3D code for supersonic inlet applications involving three-dimensional shock wave boundary layer interactions” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Computer programs - Finite volume method - Flat plates - Laminar boundary layer - Navier-Stokes equation - Shock wave interaction - Supersonic inlets - Three dimensional boundary layer - Three dimensional models - Turbulent boundary layer - Wedges
Edition Identifiers:
- The Open Library ID: OL15402776M - OL17790154M
- Online Computer Library Center (OCLC) ID: 32158036
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Validation of the RPLUS3D code for supersonic inlet applications involving three-dimensional shock wave boundary layer interactions at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
16Numerical simulation of low-density shock-wave interactions
By Christopher E. Glass
“Numerical simulation of low-density shock-wave interactions” Metadata:
- Title: ➤ Numerical simulation of low-density shock-wave interactions
- Author: Christopher E. Glass
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1999
- Publish Location: Hampton, Va - [Springfield, Va
“Numerical simulation of low-density shock-wave interactions” Subjects and Themes:
- Subjects: Computational fluid dynamics - Computerized simulation - Low density flow - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL15557231M - OL17591735M
- Online Computer Library Center (OCLC) ID: 42970345
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Numerical simulation of low-density shock-wave interactions at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
17Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6
By Scott Douglas Holland
“Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6” Metadata:
- Title: ➤ Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6
- Author: Scott Douglas Holland
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1994
- Publish Location: Hampton, Va - [Springfield, Va
“Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6” Subjects and Themes:
- Subjects: ➤ Inlet flow - Actuators - Hypersonic wind tunnels - Supersonic combustion ramjet engines - Blocking - Engine inlets - Hypersonic inlets - Cowlings - Wind tunnel tests - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL15409524M - OL18079126M
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6 at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
18Flowfield measurements in a slot-bled oblique shock wave and turbulent boundary-layer interaction
By D. O. Davis
“Flowfield measurements in a slot-bled oblique shock wave and turbulent boundary-layer interaction” Metadata:
- Title: ➤ Flowfield measurements in a slot-bled oblique shock wave and turbulent boundary-layer interaction
- Author: D. O. Davis
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Lewis Research Center
- Publish Date: 1998
- Publish Location: ➤ [Cleveland, Ohio] - Springfield, VA
“Flowfield measurements in a slot-bled oblique shock wave and turbulent boundary-layer interaction” Subjects and Themes:
- Subjects: ➤ Turbulent boundary layer - Flow measurement - Mass flow - Oblique shock waves - Boundary layer control - Boundary layer transition - Interactional aerodynamics - Slots - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL15541815M - OL17838705M
- Online Computer Library Center (OCLC) ID: 41323463
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Flowfield measurements in a slot-bled oblique shock wave and turbulent boundary-layer interaction at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
19Surface and flow field measurements in a symmetric crossing shock wave/turbulent boundary-layer interaction
By D. O. Davis
“Surface and flow field measurements in a symmetric crossing shock wave/turbulent boundary-layer interaction” Metadata:
- Title: ➤ Surface and flow field measurements in a symmetric crossing shock wave/turbulent boundary-layer interaction
- Author: D. O. Davis
- Language: English
- Number of Pages: Median: 18
- Publisher: ➤ Lewis Research Center - National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1992 - 1993
- Publish Location: ➤ Cleveland, Ohio - [Springfield, Va - [Washington, DC]
“Surface and flow field measurements in a symmetric crossing shock wave/turbulent boundary-layer interaction” Subjects and Themes:
- Subjects: Turbulent boundary layer - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL19003237M - OL14699133M
Access and General Info:
- First Year Published: 1992
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Surface and flow field measurements in a symmetric crossing shock wave/turbulent boundary-layer interaction at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
203D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
By Masashi Mizukami
“3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet” Metadata:
- Title: ➤ 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
- Author: Masashi Mizukami
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Boundary layers - Supersonic diffusers - Computational grids - Boundary layer separation - Turbulence models - Three dimensional flow - Flow distribution - Engine inlets - Internal flow - Leading edges - Shock wave interaction - Navier-Stokes equation - Shock waves
Edition Identifiers:
- The Open Library ID: OL18086923M - OL15423278M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
21Laminar and turbulent flow computations of type IV shock-shock interference aerothermal loads using unstructured grids
By Guruaja R. Vemaganti
“Laminar and turbulent flow computations of type IV shock-shock interference aerothermal loads using unstructured grids” Metadata:
- Title: ➤ Laminar and turbulent flow computations of type IV shock-shock interference aerothermal loads using unstructured grids
- Author: Guruaja R. Vemaganti
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1994
- Publish Location: Hampton, Va - [Springfield, Va
“Laminar and turbulent flow computations of type IV shock-shock interference aerothermal loads using unstructured grids” Subjects and Themes:
- Subjects: ➤ Turbulent flow - Hypersonic flow - Turbulence models - Thermal stresses - Laminar flow - Aerothermodynamics - Shock layers - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL17790648M - OL15409142M
- Online Computer Library Center (OCLC) ID: 32712246
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Laminar and turbulent flow computations of type IV shock-shock interference aerothermal loads using unstructured grids at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
22Laser light scattering by shock waves
By J. Panda
“Laser light scattering by shock waves” Metadata:
- Title: ➤ Laser light scattering by shock waves
- Author: J. Panda
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“Laser light scattering by shock waves” Subjects and Themes:
- Subjects: ➤ CCD cameras - Light scattering - Luminous intensity - Lasers - Shock waves - Laser outputs - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL17834480M - OL15498340M
- Online Computer Library Center (OCLC) ID: 39549447
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Laser light scattering by shock waves at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
23An analytical and numerical study of a shock wave interaction with an area change
By David R. Greatrix
“An analytical and numerical study of a shock wave interaction with an area change” Metadata:
- Title: ➤ An analytical and numerical study of a shock wave interaction with an area change
- Author: David R. Greatrix
- Publisher: ➤ Dept. of Aerospace Science and Engineering - Institute for Aerospace Studies
- Publish Date: 1982
- Publish Location: [Downsview, Ont.]
“An analytical and numerical study of a shock wave interaction with an area change” Subjects and Themes:
- Subjects: Shock wave interaction - Unsteady flow - One dimensional flow - Shock waves
Edition Identifiers:
- The Open Library ID: OL20982960M - OL19249029M
Access and General Info:
- First Year Published: 1982
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find An analytical and numerical study of a shock wave interaction with an area change at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
24Flow separation in shock wave boundary layer interactions at hypersonic speeds
By A. Hamed
“Flow separation in shock wave boundary layer interactions at hypersonic speeds” Metadata:
- Title: ➤ Flow separation in shock wave boundary layer interactions at hypersonic speeds
- Author: A. Hamed
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - For sale by the National Technical Information Service
- Publish Date: 1990
- Publish Location: ➤ [Springfield, Va - Washington, D.C
“Flow separation in shock wave boundary layer interactions at hypersonic speeds” Subjects and Themes:
- Subjects: ➤ Boundary layer separation - Boundary layers - Cylindrical bodies - Flat plates - Hypersonic speed - Oblique shock waves - Shock wave interaction - Turbulent boundary layer
Edition Identifiers:
- The Open Library ID: OL16126865M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Flow separation in shock wave boundary layer interactions at hypersonic speeds at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
25Studies of shock wave interactions with homogeneous and isotropic turbulence
“Studies of shock wave interactions with homogeneous and isotropic turbulence” Metadata:
- Title: ➤ Studies of shock wave interactions with homogeneous and isotropic turbulence
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: Hampton, Va - Springfield, VA
“Studies of shock wave interactions with homogeneous and isotropic turbulence” Subjects and Themes:
- Subjects: ➤ Turbulent flow - Compressible flow - Homogeneous turbulence - Isotropic turbulence - Mach number - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL17839158M
- Online Computer Library Center (OCLC) ID: 41868338
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Studies of shock wave interactions with homogeneous and isotropic turbulence at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
26The design and development of a wave interaction tube for the study of non-linear waves
By I.I Glass
“The design and development of a wave interaction tube for the study of non-linear waves” Metadata:
- Title: ➤ The design and development of a wave interaction tube for the study of non-linear waves
- Author: I.I Glass
- Number of Pages: Median: 184
- Publisher: [Institute of Aerophysics]
- Publish Date: 1950
- Publish Location: [Downsview, Ont.]
“The design and development of a wave interaction tube for the study of non-linear waves” Subjects and Themes:
- Subjects: Shock wave interaction - Shock waves
Edition Identifiers:
- The Open Library ID: OL22344503M
Access and General Info:
- First Year Published: 1950
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find The design and development of a wave interaction tube for the study of non-linear waves at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
27A time-accurate adaptive grid method and the numerical simulation of a shock-vortex interaction
By Michael J. Bockelie
“A time-accurate adaptive grid method and the numerical simulation of a shock-vortex interaction” Metadata:
- Title: ➤ A time-accurate adaptive grid method and the numerical simulation of a shock-vortex interaction
- Author: Michael J. Bockelie
- Number of Pages: Median: 17
- Publisher: Langley Research Center
- Publish Date: 1990
- Publish Location: Hampton, Va
“A time-accurate adaptive grid method and the numerical simulation of a shock-vortex interaction” Subjects and Themes:
- Subjects: Grid generation - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL21041778M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find A time-accurate adaptive grid method and the numerical simulation of a shock-vortex interaction at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
28Hydrogen file cooling with incident and swept-shock interactions in a Mach 6.4 nitrogen free stream
By George C. Olsen
“Hydrogen file cooling with incident and swept-shock interactions in a Mach 6.4 nitrogen free stream” Metadata:
- Title: ➤ Hydrogen file cooling with incident and swept-shock interactions in a Mach 6.4 nitrogen free stream
- Author: George C. Olsen
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Hydrogen file cooling with incident and swept-shock interactions in a Mach 6.4 nitrogen free stream” Subjects and Themes:
- Subjects: ➤ Hypersonic flow - Cold flow tests - Free flow - Supersonic combustion ramjet engines - Film cooling - Mass flow rate - Coolants - Oblique shock waves - Thermal protection - Gas flow - Two dimensional models - Hydrogen - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL15416715M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Hydrogen file cooling with incident and swept-shock interactions in a Mach 6.4 nitrogen free stream at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
29A numerical study of fundamental shock noise mechanisms
By Kristine R. Meadows
“A numerical study of fundamental shock noise mechanisms” Metadata:
- Title: ➤ A numerical study of fundamental shock noise mechanisms
- Author: Kristine R. Meadows
- Language: English
- Publisher: ➤ National Technical Information Service, distributor] - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“A numerical study of fundamental shock noise mechanisms” Subjects and Themes:
- Subjects: ➤ Lighthill method - Numerical analysis - Aeroacoustics - Unsteady aerodynamics - Noise prediction - Supersonic jet flow - Jet aircraft noise - Aerodynamic noise - Sound generators - Unsteady flow - Shock wave interaction - Shock wave propagation - Shock waves
Edition Identifiers:
- The Open Library ID: OL15413555M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find A numerical study of fundamental shock noise mechanisms at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
30Numerical calculations of shock-wave/boundary-layer flow interactions
By P. G. Huang
“Numerical calculations of shock-wave/boundary-layer flow interactions” Metadata:
- Title: ➤ Numerical calculations of shock-wave/boundary-layer flow interactions
- Author: P. G. Huang
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va
“Numerical calculations of shock-wave/boundary-layer flow interactions” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Turbulent flow - Corner flow - Boundary layer flow - K-epsilon turbulence model - Interactional aerodynamics - Supersonic flow - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL15419320M
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Numerical calculations of shock-wave/boundary-layer flow interactions at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
31Interaction of a shock with a longitudinal vortex
By Gordon Erlebacher
“Interaction of a shock with a longitudinal vortex” Metadata:
- Title: ➤ Interaction of a shock with a longitudinal vortex
- Author: Gordon Erlebacher
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - Institute for Computer Applications in Science and Engineering, NASA Langley Research Center
- Publish Date: 1996
- Publish Location: [Springfield, Va - Hampton, VA
“Interaction of a shock with a longitudinal vortex” Subjects and Themes:
- Subjects: ➤ Mach number - Shock wave interaction - Essentially non-oscillatory schemes - Vortex breakdown - Vortices
Edition Identifiers:
- The Open Library ID: OL15504905M
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Interaction of a shock with a longitudinal vortex at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
32A Cartesian grid approach with hierarchical refinement for compressible flows
By James J. Quirk
“A Cartesian grid approach with hierarchical refinement for compressible flows” Metadata:
- Title: ➤ A Cartesian grid approach with hierarchical refinement for compressible flows
- Author: James J. Quirk
- Language: English
- Publisher: ➤ Institute for Computer Applications in Science and Engineering, NASA Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: [Springfield, Va - Hampton, VA
“A Cartesian grid approach with hierarchical refinement for compressible flows” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Grid generation (Mathematics) - Compressible flow - Computational grids - Two dimensional flow - Cartesian coordinates - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL15404031M
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find A Cartesian grid approach with hierarchical refinement for compressible flows at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
33On the dynamics of a shock-bubble interaction
By James J. Quirk
“On the dynamics of a shock-bubble interaction” Metadata:
- Title: ➤ On the dynamics of a shock-bubble interaction
- Author: James J. Quirk
- Language: English
- Publisher: ➤ Institute for Computer Applications in Science and Engineering, NASA Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: [Springfield, Va - Hampton, VA
“On the dynamics of a shock-bubble interaction” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Computerized simulation - Computational grids - Discrete functions - Flow visualization - Grid generation (Mathematics) - Bubbles - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL15411256M
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find On the dynamics of a shock-bubble interaction at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
34The design of a wave interaction tube
By I. I. Glass
“The design of a wave interaction tube” Metadata:
- Title: ➤ The design of a wave interaction tube
- Author: I. I. Glass
- Number of Pages: Median: 136
- Publisher: Institute for Aerophysics
- Publish Date: 1950
- Publish Location: [Downsview, Ont.]
“The design of a wave interaction tube” Subjects and Themes:
- Subjects: Shock tubes - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL19114084M
Access and General Info:
- First Year Published: 1950
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find The design of a wave interaction tube at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
35Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6
By Scott D. Holland
“Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6” Metadata:
- Title: ➤ Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6
- Author: Scott D. Holland
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: [Springfield, Va - Hampton, Va
“Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6” Subjects and Themes:
- Subjects: ➤ Inlet flow - Actuators - Hypersonic wind tunnels - Supersonic combustion ramjet engines - Blocking - Engine inlets - Hypersonic inlets - Cowlings - Wind tunnel tests - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL17114738M
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6 at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
36Low dissipative high order shock-capturing methods using characteristic-based filters
By H. C. Yee
“Low dissipative high order shock-capturing methods using characteristic-based filters” Metadata:
- Title: ➤ Low dissipative high order shock-capturing methods using characteristic-based filters
- Author: H. C. Yee
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - Research Institute for Advanced Computer Science, NASA Ames Research Center
- Publish Date: 1998
- Publish Location: ➤ [Moffett Field, Calif.] - [Springfield, Va
“Low dissipative high order shock-capturing methods using characteristic-based filters” Subjects and Themes:
- Subjects: ➤ TVD schemes - Spatial resolution - Turbulent flow - Dissipation - Essentially non-oscillatory schemes - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL15544975M
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Low dissipative high order shock-capturing methods using characteristic-based filters at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
37Effect of fin leading edge sweep on shock-shock interaction at Mach 6
By Scott A. Berry
“Effect of fin leading edge sweep on shock-shock interaction at Mach 6” Metadata:
- Title: ➤ Effect of fin leading edge sweep on shock-shock interaction at Mach 6
- Author: Scott A. Berry
- Language: English
- Publisher: ➤ American Institute of Aeronautics and Astronautics - [National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ Springfield, Va - Washington, DC
“Effect of fin leading edge sweep on shock-shock interaction at Mach 6” Subjects and Themes:
- Subjects: Reynolds number - Wind tunnel tests - Leading edge sweep - Hypersonic speed - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL15501765M
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Effect of fin leading edge sweep on shock-shock interaction at Mach 6 at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
38Cylindrical sound wave generated by shock-vortex interaction
By Herbert S. Ribner
“Cylindrical sound wave generated by shock-vortex interaction” Metadata:
- Title: ➤ Cylindrical sound wave generated by shock-vortex interaction
- Author: Herbert S. Ribner
- Number of Pages: Median: 1715
- Publisher: Sine nomine
- Publish Date: 1985
- Publish Location: [S.l.]
“Cylindrical sound wave generated by shock-vortex interaction” Subjects and Themes:
- Subjects: Sound waves - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL20984705M
Access and General Info:
- First Year Published: 1985
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Cylindrical sound wave generated by shock-vortex interaction at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
39Spectrum of noise from shock-turbulence interaction
By Herbert S. Ribner
“Spectrum of noise from shock-turbulence interaction” Metadata:
- Title: ➤ Spectrum of noise from shock-turbulence interaction
- Author: Herbert S. Ribner
- Publisher: Sine nomine
- Publish Date: 1986
- Publish Location: [S.l.]
“Spectrum of noise from shock-turbulence interaction” Subjects and Themes:
- Subjects: Noise spectra - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL20984701M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Spectrum of noise from shock-turbulence interaction at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
40Numerical investigation of separated transonic turbulent flows with a multiple-time-scale turbulence model
By S. W. Kim
“Numerical investigation of separated transonic turbulent flows with a multiple-time-scale turbulence model” Metadata:
- Title: ➤ Numerical investigation of separated transonic turbulent flows with a multiple-time-scale turbulence model
- Author: S. W. Kim
- Language: English
- Number of Pages: Median: 38
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration
- Publish Date: 1990
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“Numerical investigation of separated transonic turbulent flows with a multiple-time-scale turbulence model” Subjects and Themes:
- Subjects: ➤ Turbulent flow - Turbulent boundary layer - Separated flow - Transonic flow - Turbulence models - Compressible flow - Turbulence - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL16128063M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Numerical investigation of separated transonic turbulent flows with a multiple-time-scale turbulence model at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
41Computational modeling and validation for hypersonic inlets
By Louis A. Povinelli
“Computational modeling and validation for hypersonic inlets” Metadata:
- Title: ➤ Computational modeling and validation for hypersonic inlets
- Author: Louis A. Povinelli
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration
- Publish Date: 1990
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“Computational modeling and validation for hypersonic inlets” Subjects and Themes:
- Subjects: ➤ Aerodynamics, Hypersonic - Coputational fluid dynamics - Hypersonic Aerodynamics - Hypersonic inlets - Inlet flow - Navier-Stokes equation - Research - Shock wave interaction - Turbulence models
- Places: United States
Edition Identifiers:
- The Open Library ID: OL16127973M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Computational modeling and validation for hypersonic inlets at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
42Internal aerodynamics of a generic three-dimensional scramjet inlet at Mach 10
By Scott Douglas Holland
“Internal aerodynamics of a generic three-dimensional scramjet inlet at Mach 10” Metadata:
- Title: ➤ Internal aerodynamics of a generic three-dimensional scramjet inlet at Mach 10
- Author: Scott Douglas Holland
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center - NASA Center for AeroSpace Information, distributor
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - Hampton, Va - Linthicum Heights, MD
“Internal aerodynamics of a generic three-dimensional scramjet inlet at Mach 10” Subjects and Themes:
- Subjects: ➤ Inlet flow - Engine design - Hypersonic inlets - Wind tunnel tests - Supersonic combustion ramjet engines - Flow distribution - Hypersonic speed - Internal flow - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL15412088M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Internal aerodynamics of a generic three-dimensional scramjet inlet at Mach 10 at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
43Mach 10 computational study of a three-dimensional scramjet inlet flow field
By Scott Douglas Holland
“Mach 10 computational study of a three-dimensional scramjet inlet flow field” Metadata:
- Title: ➤ Mach 10 computational study of a three-dimensional scramjet inlet flow field
- Author: Scott Douglas Holland
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1995
- Publish Location: Hampton, Va - [Springfield, Va
“Mach 10 computational study of a three-dimensional scramjet inlet flow field” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Inlet flow - Computational grids - Aerodynamics - Three dimensional flow - Supersonic combustion ramjet engines - Navier-Stokes equation - Hypersonic speed - Supersonic inlets - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL15410430M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Mach 10 computational study of a three-dimensional scramjet inlet flow field at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
44Weak-wave analysis of shock interaction with a slipstream
By Raymond L. Barger
“Weak-wave analysis of shock interaction with a slipstream” Metadata:
- Title: ➤ Weak-wave analysis of shock interaction with a slipstream
- Author: Raymond L. Barger
- Number of Pages: Median: 17
- Publisher: Langley Research Center
- Publish Date: 1988
- Publish Location: Hampton, Va
“Weak-wave analysis of shock interaction with a slipstream” Subjects and Themes:
- Subjects: Slipstreams - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL18927212M
Author's Alternative Names:
"Raymond L Barger"Access and General Info:
- First Year Published: 1988
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Weak-wave analysis of shock interaction with a slipstream at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
45Experimental studies of shock-wave/wall-jet interaction in hypersonic flow
By Michael S. Holden
“Experimental studies of shock-wave/wall-jet interaction in hypersonic flow” Metadata:
- Title: ➤ Experimental studies of shock-wave/wall-jet interaction in hypersonic flow
- Author: Michael S. Holden
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1994
- Publish Location: Hampton, Va - [Springfield, Va
“Experimental studies of shock-wave/wall-jet interaction in hypersonic flow” Subjects and Themes:
- Subjects: ➤ Turbulent flow - Hypersonic flow - Wind tunnel tests - Nozzle flow - Film cooling - Wall jets - Shock wave interaction - Shock waves
Edition Identifiers:
- The Open Library ID: OL17000207M
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Experimental studies of shock-wave/wall-jet interaction in hypersonic flow at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
46Shock wave interaction with an abrupt area change
By M. D. Salas
“Shock wave interaction with an abrupt area change” Metadata:
- Title: ➤ Shock wave interaction with an abrupt area change
- Author: M. D. Salas
- Language: English
- Number of Pages: Median: 13
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1991
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va
“Shock wave interaction with an abrupt area change” Subjects and Themes:
- Subjects: ➤ Mathematical models - Shock waves - Computational fluid dynamics - Numerical analysis - Uniqueness theorem - Entropy - Euler equations of motion - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL16135216M
Access and General Info:
- First Year Published: 1991
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Shock wave interaction with an abrupt area change at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
47Numerical simulation of supersonic flow using a new analytical bleed boundary condition
By G. J. Harloff
“Numerical simulation of supersonic flow using a new analytical bleed boundary condition” Metadata:
- Title: ➤ Numerical simulation of supersonic flow using a new analytical bleed boundary condition
- Author: G. J. Harloff
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Numerical simulation of supersonic flow using a new analytical bleed boundary condition” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Supersonic boundary layers - Supersonic flow - Flow distribution - Oblique shock waves - Boundary layer control - Supersonic inlets - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL15381444M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Numerical simulation of supersonic flow using a new analytical bleed boundary condition at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
48Interactive calculation procedures for mixed compression inlets
By Eli Reshotko
“Interactive calculation procedures for mixed compression inlets” Metadata:
- Title: ➤ Interactive calculation procedures for mixed compression inlets
- Author: Eli Reshotko
- Language: English
- Publisher: ➤ Dept. of Mechanical and Aerospace Engineering, School of Engineering, Case Institute of Technology, Case Western Reserve University
- Publish Date: 1983
- Publish Location: Cleveland, Ohio
“Interactive calculation procedures for mixed compression inlets” Subjects and Themes:
- Subjects: ➤ Supersonic aircraft - Laminar boundary layer - Turbulent boundary layer - Shock wave interaction - Oblique shock waves - Nacelles
Edition Identifiers:
- The Open Library ID: OL16125496M
Access and General Info:
- First Year Published: 1983
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Interactive calculation procedures for mixed compression inlets at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
49Interaction of oblique shock and detonation waves
By Y. Sheng
“Interaction of oblique shock and detonation waves” Metadata:
- Title: ➤ Interaction of oblique shock and detonation waves
- Author: Y. Sheng
- Publisher: ➤ Institute for Aerospace Studies
- Publish Date: 1982
- Publish Location: [Downsview, Ont.]
“Interaction of oblique shock and detonation waves” Subjects and Themes:
- Subjects: Oblique shock waves - Detonation waves - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL20968198M
Access and General Info:
- First Year Published: 1982
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Interaction of oblique shock and detonation waves at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
50Numerical analysis of peak heat transfer rates for hypersonic flow over a cowl leading edge
By Jeffrey A. White
“Numerical analysis of peak heat transfer rates for hypersonic flow over a cowl leading edge” Metadata:
- Title: ➤ Numerical analysis of peak heat transfer rates for hypersonic flow over a cowl leading edge
- Author: Jeffrey A. White
- Publisher: AIAA
- Publish Date: 1987
- Publish Location: New York
“Numerical analysis of peak heat transfer rates for hypersonic flow over a cowl leading edge” Subjects and Themes:
- Subjects: Heat transfer - Hypersonic flow - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL19250730M
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Numerical analysis of peak heat transfer rates for hypersonic flow over a cowl leading edge at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.