Explore: Hypersonic Speed
Discover books, insights, and more — all in one place.
Learn more about Hypersonic Speed with top reads curated from trusted sources — all in one place.
AI-Generated Overview About “hypersonic-speed”:
Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements
By W. Lance Richards
“Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements” Metadata:
- Title: ➤ Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements
- Author: W. Lance Richards
- Language: English
- Number of Pages: Median: 14
- Publisher: ➤ Available from the NASA Center for AeroSpace Information] - National Technical Information Service, distributor] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1997
- Publish Location: ➤ [Springfield, Va - [Linthicum Heights, MD - [Washington, D.C.]
“Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements” Subjects and Themes:
- Subjects: ➤ Aerodynamics - Aerodynamics, Hypersonic - Boundary layer transition - Data processing - Design and construction - Finite element method - Hypersonic Aerodynamics - Hypersonic planes - Hypersonic speed - Leading edges - Research - Structural design
Edition Identifiers:
- The Open Library ID: OL18134772M - OL19433479M - OL15548269M - OL17132909M - OL17839410M
- Online Computer Library Center (OCLC) ID: 41975259
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 Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
2Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept
By David E. Hahne
“Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept” Metadata:
- Title: ➤ Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept
- Author: David E. Hahne
- Language: English
- Number of Pages: Median: 23
- Publisher: ➤ Available from the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Springfield, Va - Springfield, VA - Hampton, Va
“Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Aerodynamic coefficients - Aerodynamic stability - Aerodynamics, Hypersonic - Angle of attack - Hypersonic Aerodynamics - Hypersonic speed - Hypersonic vehicles - Low speed - Mach number - Pitching moments - Stability - Stability of airplanes - Stabilizers (Fluid dynamics) - Vortices - Waveriders - Wind tunnel stability tests
Edition Identifiers:
- The Open Library ID: OL18134999M - OL17133262M - OL17839424M - OL21033491M - OL15549003M
- Online Computer Library Center (OCLC) ID: 42055832
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 Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
3Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel
By Glen P. Doggett
“Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel” Metadata:
- Title: ➤ Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel
- Author: Glen P. Doggett
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: [Springfield, Va - Hampton, Va
“Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel” Subjects and Themes:
- Subjects: ➤ Boundary layer stability - Hypersonics - Aerodynamic stability - Navier-Stokes equation - Hypersonic boundary layer - Hypersonic speed - Aerodynamic noise - Zero angle of attack - Angle of attack
Edition Identifiers:
- The Open Library ID: OL18114813M - OL15487085M - OL17123234M - OL17564495M
- Online Computer Library Center (OCLC) ID: 38994217
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 Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
4Three-dimensional Navier-Stokes simulations with two-equation turbulence models of intersecting shock-waves/turbulent boundary layer at Mach 8.3
By J. E. Bardina
“Three-dimensional Navier-Stokes simulations with two-equation turbulence models of intersecting shock-waves/turbulent boundary layer at Mach 8.3” Metadata:
- Title: ➤ Three-dimensional Navier-Stokes simulations with two-equation turbulence models of intersecting shock-waves/turbulent boundary layer at Mach 8.3
- Author: J. E. Bardina
- Language: English
- Publisher: ➤ [National Aeronautics and Space Administration - American Institute of Aeronautics and Astronautics - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ Washington, D.C - Springfield, Va
“Three-dimensional Navier-Stokes simulations with two-equation turbulence models of intersecting shock-waves/turbulent boundary layer at Mach 8.3” Subjects and Themes:
- Subjects: ➤ Velocity distribution - Turbulent boundary layer - Three dimensional boundary layer - Turbulence models - Three dimensional flow - Boundary layer flow - Heat transfer - Navier-Stokes equation - Hypersonic speed - Boundary conditions - Shock waves
Edition Identifiers:
- The Open Library ID: OL15498995M - OL17125581M - OL18119023M - OL17572158M
- Online Computer Library Center (OCLC) ID: 39880013
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 Three-dimensional Navier-Stokes simulations with two-equation turbulence models of intersecting shock-waves/turbulent boundary layer at Mach 8.3 at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
5Shock-tunnel combustor testing for hypersonic vehicles
By Mark Loomis
“Shock-tunnel combustor testing for hypersonic vehicles” Metadata:
- Title: ➤ Shock-tunnel combustor testing for hypersonic vehicles
- Author: Mark Loomis
- Language: English
- Publisher: ➤ MCAT Institute - National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ Springfield, Va - San Jose, Calif - [Washington, DC
“Shock-tunnel combustor testing for hypersonic vehicles” Subjects and Themes:
- Subjects: ➤ Wind tunnel tests - Two dimensional flow - Hypersonic flow - Supersonic combustion ramjet engines - Propulsion system performance - Propulsion system configurations - Engine tests - Air breathing engines - Hypersonic speed - Combustion chambers - Hypersonic aircraft - Hypersonic inlets - Inlet nozzles - Mach number
Edition Identifiers:
- The Open Library ID: OL17001315M - OL18076085M - OL15403346M
- Online Computer Library Center (OCLC) ID: 32198098
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 Shock-tunnel combustor testing for hypersonic vehicles at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
6Separation characteristics of generic stores from lee side of an inclined flat plate at Mach 6
By Floyd J. Wilcox
“Separation characteristics of generic stores from lee side of an inclined flat plate at Mach 6” Metadata:
- Title: ➤ Separation characteristics of generic stores from lee side of an inclined flat plate at Mach 6
- Author: Floyd J. Wilcox
- Language: English
- Number of Pages: Median: 43
- Publisher: ➤ Available from the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center - For sale by the National Technical Information Service
- Publish Date: 1995
- Publish Location: ➤ Hampton, Va - Springfield, VA - [Springfield, VA
“Separation characteristics of generic stores from lee side of an inclined flat plate at Mach 6” Subjects and Themes:
- Subjects: ➤ Aerodynamic configurations - Aerodynamics, Hypersonic - Bombers - Design and construction - External store separation - External stores - Flat plates - Free flow - Hypersonic Aerodynamics - Hypersonic speed - Separated flow
Edition Identifiers:
- The Open Library ID: OL17635043M - OL16125421M - OL17803983M
- Online Computer Library Center (OCLC) ID: 60398151 - 33144596
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 Separation characteristics of generic stores from lee side of an inclined flat plate at Mach 6 at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
7Thermal analysis of a metallic wing glove for a Mach-8 boundary-layer experiment
By Leslie Gong
“Thermal analysis of a metallic wing glove for a Mach-8 boundary-layer experiment” Metadata:
- Title: ➤ Thermal analysis of a metallic wing glove for a Mach-8 boundary-layer experiment
- Author: Leslie Gong
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Dryden Flight Research Center
- Publish Date: 1998
- Publish Location: ➤ Springfield, VA - Edwards, Calif
“Thermal analysis of a metallic wing glove for a Mach-8 boundary-layer experiment” Subjects and Themes:
- Subjects: ➤ Hypersonic speed - Finite element method - Aerodynamic heating - Thermal analysis - Boundary layer transition - Design analysis
Edition Identifiers:
- The Open Library ID: OL15541774M - OL17838703M
- Online Computer Library Center (OCLC) ID: 41214761
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 Thermal analysis of a metallic wing glove for a Mach-8 boundary-layer experiment at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
8A first scramjet study
By George Emmanuel
“A first scramjet study” Metadata:
- Title: A first scramjet study
- Author: George Emmanuel
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1989
- Publish Location: ➤ [Washington, DC - Springfield, Va
“A first scramjet study” Subjects and Themes:
- Subjects: ➤ Temperature effects - Lift - Nozzle flow - Thrust - Hypersonic speed - Supersonic combustion ramjet engines
Edition Identifiers:
- The Open Library ID: OL14972502M - OL17683624M
Access and General Info:
- First Year Published: 1989
- 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 first scramjet study at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
9Mach 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.
10Hypersonic 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.
11Numerical 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.
12Inviscid flow computations of the orbital sciences X-34 over a Mach number range of 1.25 to 6.0
By Ramadas K. Prabhu
“Inviscid flow computations of the orbital sciences X-34 over a Mach number range of 1.25 to 6.0” Metadata:
- Title: ➤ Inviscid flow computations of the orbital sciences X-34 over a Mach number range of 1.25 to 6.0
- Author: Ramadas K. Prabhu
- Language: English
- Publisher: ➤ Available from NASA Center for Aerospace Information - National Aeronautics and Science Administration, Langley Research Center
- Publish Date: 2001
- Publish Location: Hampton, Va - Hanover, MD
“Inviscid flow computations of the orbital sciences X-34 over a Mach number range of 1.25 to 6.0” Subjects and Themes:
- Subjects: ➤ Inviscid flow - Viscous flow - Hypersonic speed - Aerodynamic loads - Supersonic speed - Computational fluid dynamics
Edition Identifiers:
- The Open Library ID: OL17607401M - OL17718834M
- Online Computer Library Center (OCLC) ID: 50134015
Access and General Info:
- First Year Published: 2001
- 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 Inviscid flow computations of the orbital sciences X-34 over a Mach number range of 1.25 to 6.0 at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
13Physics of interplanetary dust collection with aerogel
By William W. Anderson
“Physics of interplanetary dust collection with aerogel” Metadata:
- Title: ➤ Physics of interplanetary dust collection with aerogel
- Author: William W. Anderson
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Physics of interplanetary dust collection with aerogel” Subjects and Themes:
- Subjects: ➤ Accumulators - Cosmic dust - Interplanetary dust - Dust collectors - Hypersonic speed - Hypoersonic speed
Edition Identifiers:
- The Open Library ID: OL15507765M - OL17839128M
- Online Computer Library Center (OCLC) ID: 40493499
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 Physics of interplanetary dust collection with aerogel at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
14Recent flight test results of the joint CIAM-NASA Mach 6.5 Scramjet Flight Program
By Alexander S. Roudakov
“Recent flight test results of the joint CIAM-NASA Mach 6.5 Scramjet Flight Program” Metadata:
- Title: ➤ Recent flight test results of the joint CIAM-NASA Mach 6.5 Scramjet Flight Program
- Author: Alexander S. Roudakov
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: ➤ Edwards, Calif - Springfield, VA
“Recent flight test results of the joint CIAM-NASA Mach 6.5 Scramjet Flight Program” Subjects and Themes:
- Subjects: ➤ Missiles - Supersonic combustion - Airborne equipment - Hypersonic speed - Supersonic combustion ramjet engines - Flight tests - Launching
Edition Identifiers:
- The Open Library ID: OL17583619M - OL15548793M
- Online Computer Library Center (OCLC) ID: 41942401
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 Recent flight test results of the joint CIAM-NASA Mach 6.5 Scramjet Flight Program at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
15Parametric study of shock-induced combustion in a hydrogen air system
By J. K. Ahuja
“Parametric study of shock-induced combustion in a hydrogen air system” Metadata:
- Title: ➤ Parametric study of shock-induced combustion in a hydrogen air system
- Author: J. K. Ahuja
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - NASA Langley Research Center - Institute for Computational and Applied Mechanics, Old Dominion University
- Publish Date: 1994
- Publish Location: ➤ Hampton, Va - Norfolk, Va - [Springfield, Va
“Parametric study of shock-induced combustion in a hydrogen air system” Subjects and Themes:
- Subjects: ➤ Combustion physics - Wave interaction - Mathematical models - Free flow - Activation energy - Blunt bodies - Hypersonic speed - Shock heating
Edition Identifiers:
- The Open Library ID: OL15409433M
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 Parametric study of shock-induced combustion in a hydrogen air system at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
16Flow 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.
17The NASA Hyper-X Program
By D. Freeman
“The NASA Hyper-X Program” Metadata:
- Title: The NASA Hyper-X Program
- Author: D. Freeman
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor - International Astronautical Federation
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - Paris, France - [Washington, D.C
“The NASA Hyper-X Program” Subjects and Themes:
- Subjects: Air breathing engines - Hypersonic speed - Data bases - Technologies - Hypersonic vehicles
Edition Identifiers:
- The Open Library ID: OL17583214M
- Online Computer Library Center (OCLC) ID: 41994964
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 The NASA Hyper-X Program at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
18Application of CFD to the analysis and design of high-speed inlets
By William C. Rose
“Application of CFD to the analysis and design of high-speed inlets” Metadata:
- Title: ➤ Application of CFD to the analysis and design of high-speed inlets
- Author: William C. Rose
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Application of CFD to the analysis and design of high-speed inlets” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Engine design - Histories - Engine inlets - Hypersonic speed - Computer aided design - Computer programs - High speed
Edition Identifiers:
- The Open Library ID: OL15413873M
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 Application of CFD to the analysis and design of high-speed inlets at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
19Computational study of flow establishment in hypersonic pulse facilities
By Shaye Yungster
“Computational study of flow establishment in hypersonic pulse facilities” Metadata:
- Title: ➤ Computational study of flow establishment in hypersonic pulse facilities
- Author: Shaye Yungster
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Cleveland, Ohio] - [Springfield, Va
“Computational study of flow establishment in hypersonic pulse facilities” Subjects and Themes:
- Subjects: ➤ Combustion physics - Computational fluid dynamics - Detonation waves - TVD schemes - Flammable gases - Temporal distribution - Flow distribution - Backward differencing - Hypervelocity projectiles - Hypersonic speed - Reacting flow - Ram accelerators
Edition Identifiers:
- The Open Library ID: OL15423158M
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 Computational study of flow establishment in hypersonic pulse facilities at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
20On the Gortler vortex instability mechanism at hypersonic speeds
By Philip Hall
“On the Gortler vortex instability mechanism at hypersonic speeds” Metadata:
- Title: ➤ On the Gortler vortex instability mechanism at hypersonic speeds
- Author: Philip Hall
- Number of Pages: Median: 26
- Publisher: ICASE
- Publish Date: 1989
- Publish Location: Hampton, Va
“On the Gortler vortex instability mechanism at hypersonic speeds” Subjects and Themes:
- Subjects: Hypersonic speed - Gortler vortices
Edition Identifiers:
- The Open Library ID: OL19379741M
Access and General Info:
- First Year Published: 1989
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find On the Gortler vortex instability mechanism at hypersonic speeds at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
21Transition at hypersonic speeds
By Mark Vladimir Morkovin
“Transition at hypersonic speeds” Metadata:
- Title: ➤ Transition at hypersonic speeds
- Author: Mark Vladimir Morkovin
- Number of Pages: Median: 24
- Publisher: ICASE
- Publish Date: 1987
- Publish Location: Hampton, Va
“Transition at hypersonic speeds” Subjects and Themes:
- Subjects: Transition - Hypersonic speed
Edition Identifiers:
- The Open Library ID: OL19003085M
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 Transition at hypersonic speeds at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
22Supersonic wind tunnel tests of a half-axisymmetric 12⁰-spike inlet to a rocket-based combined-cycle propulsion system
By J. R. DeBonis
“Supersonic wind tunnel tests of a half-axisymmetric 12⁰-spike inlet to a rocket-based combined-cycle propulsion system” Metadata:
- Title: ➤ Supersonic wind tunnel tests of a half-axisymmetric 12⁰-spike inlet to a rocket-based combined-cycle propulsion system
- Author: J. R. DeBonis
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Glenn Research Center - Available from NASA Center for Aerospace Information
- Publish Date: 2001
- Publish Location: ➤ Hanover, MD - [Cleveland, Ohio]
“Supersonic wind tunnel tests of a half-axisymmetric 12⁰-spike inlet to a rocket-based combined-cycle propulsion system” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Air breathing boosters - Pressure distribution - Propulsion - Wind tunnel tests - Hypersonic speed
Edition Identifiers:
- The Open Library ID: OL16028849M
Access and General Info:
- First Year Published: 2001
- 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 Supersonic wind tunnel tests of a half-axisymmetric 12⁰-spike inlet to a rocket-based combined-cycle propulsion system at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
23Effect 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.
24On the instability of hypersonic flow past a flat plate
By Nicholas Blackaby
“On the instability of hypersonic flow past a flat plate” Metadata:
- Title: ➤ On the instability of hypersonic flow past a flat plate
- Author: Nicholas Blackaby
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1990
- Publish Location: Hampton, Va
“On the instability of hypersonic flow past a flat plate” Subjects and Themes:
- Subjects: ➤ Hypersonic boundary layer - Flat plates - Vorticity - Boundary layer stability - Hypersonic flow - Hypersonic speed - Boundary layer flow
Edition Identifiers:
- The Open Library ID: OL16125582M
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 On the instability of hypersonic flow past a flat plate at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
25Turbulence modeling
By Jorge E. Bardina
“Turbulence modeling” Metadata:
- Title: Turbulence modeling
- Author: Jorge E. Bardina
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“Turbulence modeling” Subjects and Themes:
- Subjects: ➤ Computerized simulation - Hypersonic flow - Turbulence models - Program verification (Computers) - Navier-Stokes equation - Separated flow - Hypersonic speed - Computer aided design - Computer programs - Compressibility - Transition flow - Hypersonic shock
Edition Identifiers:
- The Open Library ID: OL15413741M
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 Turbulence modeling at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
26Computational study of a McDonnell Douglas single-stage-to-orbit vehicle concept for aerodynamic analysis
By Ramadas K. Prabhu
“Computational study of a McDonnell Douglas single-stage-to-orbit vehicle concept for aerodynamic analysis” Metadata:
- Title: ➤ Computational study of a McDonnell Douglas single-stage-to-orbit vehicle concept for aerodynamic analysis
- Author: Ramadas K. Prabhu
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1996
- Publish Location: Hampton, Va - [Springfield, Va
“Computational study of a McDonnell Douglas single-stage-to-orbit vehicle concept for aerodynamic analysis” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Applications programs (Computers) - Computational grids - Finite element method - Hypersonic flow - Hypersonic speed - Inviscid flow - Single stage to orbit vehicles - Unstructured grids (Mathematics)
Edition Identifiers:
- The Open Library ID: OL15487206M
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 Computational study of a McDonnell Douglas single-stage-to-orbit vehicle concept for aerodynamic analysis at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
27Inviscid flow computations of the shuttle orbiter for Mach 10 and 15 and angle of attack 40 to 60 degrees
By Ramadas K. Prabhu
“Inviscid flow computations of the shuttle orbiter for Mach 10 and 15 and angle of attack 40 to 60 degrees” Metadata:
- Title: ➤ Inviscid flow computations of the shuttle orbiter for Mach 10 and 15 and angle of attack 40 to 60 degrees
- Author: Ramadas K. Prabhu
- Language: English
- Publisher: ➤ Available from NASA Center for Aerospace Information - National Aeronautics and Science Administration, Langley Research Center
- Publish Date: 2001
- Publish Location: Hampton, Va - Hanover, MD
“Inviscid flow computations of the shuttle orbiter for Mach 10 and 15 and angle of attack 40 to 60 degrees” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Inviscid flow - Aerodynamic coefficients - Space shuttle orbiters - Angle of attack - Hypersonic speed - Aerodynamic characteristics - Mach number
Edition Identifiers:
- The Open Library ID: OL16042466M
Access and General Info:
- First Year Published: 2001
- 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 Inviscid flow computations of the shuttle orbiter for Mach 10 and 15 and angle of attack 40 to 60 degrees at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
28Internal 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.
29Mach 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.
30Multiphysics simulation of active hypersonic lip cooling
By Matthew E. Melis
“Multiphysics simulation of active hypersonic lip cooling” Metadata:
- Title: ➤ Multiphysics simulation of active hypersonic lip cooling
- Author: Matthew E. Melis
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 1999
- Publish Location: ➤ [Cleveland, Ohio] - [Springfield, Va
“Multiphysics simulation of active hypersonic lip cooling” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Aerothermodynamics - Hypersonic speed - Temperature profiles - Computerized simulation - Surface temperature
Edition Identifiers:
- The Open Library ID: OL15563038M
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 Multiphysics simulation of active hypersonic lip cooling at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
31Mach 5 to 7 RBCC propulsion system testing at NASA-LeRC HTF
By H. Douglas Perkins
“Mach 5 to 7 RBCC propulsion system testing at NASA-LeRC HTF” Metadata:
- Title: ➤ Mach 5 to 7 RBCC propulsion system testing at NASA-LeRC HTF
- Author: H. Douglas Perkins
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Mach 5 to 7 RBCC propulsion system testing at NASA-LeRC HTF” Subjects and Themes:
- Subjects: Engine tests - Hypersonic wind tunnels - Hypersonic speed - Integral rocket ramjets
Edition Identifiers:
- The Open Library ID: OL15497561M
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 Mach 5 to 7 RBCC propulsion system testing at NASA-LeRC HTF at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
32Spectral solution of the viscous blunt body problem
By David A. Kopriva
“Spectral solution of the viscous blunt body problem” Metadata:
- Title: ➤ Spectral solution of the viscous blunt body problem
- Author: David A. Kopriva
- 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
“Spectral solution of the viscous blunt body problem” Subjects and Themes:
- Subjects: ➤ Viscous flow - Chebyshev approximation - Computational grids - Collocation - Blunt bodies - Spectral methods - Hypersonic speed
Edition Identifiers:
- The Open Library ID: OL15409737M
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 Spectral solution of the viscous blunt body problem at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
33Mach 6 flow field surveys beneath the forebody of an airbreathing missile
By Patrick J. Johnston
“Mach 6 flow field surveys beneath the forebody of an airbreathing missile” Metadata:
- Title: ➤ Mach 6 flow field surveys beneath the forebody of an airbreathing missile
- Author: Patrick J. Johnston
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service
- Publish Date: 1986
- Publish Location: ➤ [Washington, D.C.] - Springfield, Va
“Mach 6 flow field surveys beneath the forebody of an airbreathing missile” Subjects and Themes:
- Subjects: ➤ Missiles - Boundary layers - Reynolds number - Wind tunnel tests - Flow distribution - Air breathing boosters - Hypersonic speed - Mach number
Edition Identifiers:
- The Open Library ID: OL16114957M
Access and General Info:
- First Year Published: 1986
- 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 6 flow field surveys beneath the forebody of an airbreathing missile at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
34Nonlinear potential analysis techniques for supersonic/hypersonic aerodynamic design
By V. Shankar
“Nonlinear potential analysis techniques for supersonic/hypersonic aerodynamic design” Metadata:
- Title: ➤ Nonlinear potential analysis techniques for supersonic/hypersonic aerodynamic design
- Author: V. Shankar
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - Rockwell International Corporation
- Publish Date: 1984
- Publish Location: ➤ Hampton, Va - Los Angeles, Calif
“Nonlinear potential analysis techniques for supersonic/hypersonic aerodynamic design” Subjects and Themes:
- Subjects: ➤ Aerodynamic configurations - Hypersonic Aerodynamics - Hypersonic speed - Inviscid flow - Nonlinear equations - Potential theory - Supersonic Aerodynamics - Supersonic speed
Edition Identifiers:
- The Open Library ID: OL16154917M
Access and General Info:
- First Year Published: 1984
- 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 Nonlinear potential analysis techniques for supersonic/hypersonic aerodynamic design at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
35Transition at hypersonic speeds
By Mark Vladimir Morkovin
“Transition at hypersonic speeds” Metadata:
- Title: ➤ Transition at hypersonic speeds
- Author: Mark Vladimir Morkovin
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - Institute for Computer Applications in Science and Engineering, NASA Langley Research Center
- Publish Date: 1987
- Publish Location: Hampton, Va - [Springfield, Va
“Transition at hypersonic speeds” Subjects and Themes:
- Subjects: Flow stability - Heat transfer - Hypersonic speed - Numerical analysis - Transition flow
Edition Identifiers:
- The Open Library ID: OL15408354M
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 Transition at hypersonic speeds at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.