Explore: Transonic Speed
Discover books, insights, and more — all in one place.
Learn more about Transonic Speed with top reads curated from trusted sources — all in one place.
AI-Generated Overview About “transonic-speed”:
Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1Two-dimensional converging-diverging rippled nozzles at transonic speeds
By John R. Carlson
“Two-dimensional converging-diverging rippled nozzles at transonic speeds” Metadata:
- Title: ➤ Two-dimensional converging-diverging rippled nozzles at transonic speeds
- Author: John R. Carlson
- Language: English
- Number of Pages: Median: 105
- Publisher: ➤ Langley Research Center - National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1994
- Publish Location: ➤ Hampton - Hampton, Va - [Springfield, Va
“Two-dimensional converging-diverging rippled nozzles at transonic speeds” Subjects and Themes:
- Subjects: ➤ Convergent-divergent nozzles - Discharge coefficient - Drag - Nozzle flow - Nozzle geometry - Nozzles - Ripples - Thrust - Trailing edges - Transonic speed - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: ➤ OL19752932M - OL16487219M - OL15403665M - OL16982124M - OL19753709M - OL18076297M
- Online Computer Library Center (OCLC) ID: 32220800
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 Two-dimensional converging-diverging rippled nozzles at transonic speeds at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
2Cavity unsteady-pressure measurements at subsonic and transonic speeds
By Maureen B. Tracy
“Cavity unsteady-pressure measurements at subsonic and transonic speeds” Metadata:
- Title: ➤ Cavity unsteady-pressure measurements at subsonic and transonic speeds
- Author: Maureen B. Tracy
- Language: English
- Number of Pages: Median: 72
- Publisher: ➤ National Technical Information Service, distributor - Available from National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1997
- Publish Location: Hampton, Va - Springfield, VA
“Cavity unsteady-pressure measurements at subsonic and transonic speeds” Subjects and Themes:
- Subjects: ➤ Cavitation - Cavity flow - Cavity resonators - Measurement - Pressure - Pressure measurement - Subsonic speed - Transonic Aerodynamics - Transonic speed - Unsteady flow - Unsteady flow (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL17135029M - OL17591846M - OL15548837M - OL19158930M - OL18134951M
- Online Computer Library Center (OCLC) ID: 42677336
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 Cavity unsteady-pressure measurements at subsonic and transonic speeds at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
3In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisions with contemporary aircraft)
By Edwin J. Saltzman
“In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisions with contemporary aircraft)” Metadata:
- Title: ➤ In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisions with contemporary aircraft)
- Author: Edwin J. Saltzman
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program - National Technical Information Service, distributor]
- Publish Date: 1994
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisions with contemporary aircraft)” Subjects and Themes:
- Subjects: ➤ X-29 aircraft - Wave drag - Lift - Airfoil profiles - Swept forward wings - Drag - Transonic speed
Edition Identifiers:
- The Open Library ID: OL18080007M - OL17008295M - OL15411782M
- Online Computer Library Center (OCLC) ID: 32938383
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 In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisions with contemporary aircraft) at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
4Pitot-pressure measurements in flow fields behind a rectangular nozzle with exhaust jet for free-stream mach numbers of 0.00, 0,60, and 1.20
By Lawrence E. Putnam
“Pitot-pressure measurements in flow fields behind a rectangular nozzle with exhaust jet for free-stream mach numbers of 0.00, 0,60, and 1.20” Metadata:
- Title: ➤ Pitot-pressure measurements in flow fields behind a rectangular nozzle with exhaust jet for free-stream mach numbers of 0.00, 0,60, and 1.20
- Author: Lawrence E. Putnam
- Language: English
- Number of Pages: Median: 151
- Publisher: ➤ National Technical Information Service, distributor] - Langley Research Center - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1986
- Publish Location: ➤ [Washington, DC] - [Springfield, Va - Hampton, Va
“Pitot-pressure measurements in flow fields behind a rectangular nozzle with exhaust jet for free-stream mach numbers of 0.00, 0,60, and 1.20” Subjects and Themes:
- Subjects: ➤ Exhaust nozzles - Flow distribution - Free flow - Jet exhaust - Mach number - Nozzles - Pitot tubes - Pressure measurement - Transonic speed
Edition Identifiers:
- The Open Library ID: OL20985250M - OL18083203M - OL15417483M
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 Pitot-pressure measurements in flow fields behind a rectangular nozzle with exhaust jet for free-stream mach numbers of 0.00, 0,60, and 1.20 at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
5Effect of empennage arrangement on single engine nozzle/afterbody static pressures at transonic speeds
By William P. Henderson
“Effect of empennage arrangement on single engine nozzle/afterbody static pressures at transonic speeds” Metadata:
- Title: ➤ Effect of empennage arrangement on single engine nozzle/afterbody static pressures at transonic speeds
- Author: William P. Henderson
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service] - Langley Research Center - National Aeronautics and Space Administration, Scientific and Technical Information Division
- Publish Date: 1987 - 1988
- Publish Location: ➤ [Washington, DC] - Hampton, Va - [Springfield, Va
“Effect of empennage arrangement on single engine nozzle/afterbody static pressures at transonic speeds” Subjects and Themes:
- Subjects: Aerodynamics, Transonic - Nozzles - Tail assemblies - Transonic Aerodynamics - Transonic speed
Edition Identifiers:
- The Open Library ID: OL19250322M - OL14664598M
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 Effect of empennage arrangement on single engine nozzle/afterbody static pressures at transonic speeds at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
6Measurements of unsteady pressure and structural response for an elastic supercritical wing
By Clinton V. Eckstrom
“Measurements of unsteady pressure and structural response for an elastic supercritical wing” Metadata:
- Title: ➤ Measurements of unsteady pressure and structural response for an elastic supercritical wing
- Author: Clinton V. Eckstrom
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - For sale by the National Technical Information Service
- Publish Date: 1994
- Publish Location: ➤ Hampton - Hampton, Va - [Springfield, Va
“Measurements of unsteady pressure and structural response for an elastic supercritical wing” Subjects and Themes:
- Subjects: ➤ Aeroelasticity - Dynamic response - Pressure distribution - Supercritical wings - Transonic speed - Unsteady flow - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL15410960M - OL17790670M - OL22824033M
- Online Computer Library Center (OCLC) ID: 32863973
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 Measurements of unsteady pressure and structural response for an elastic supercritical wing at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
7Validation of the NPARC code for nozzle afterbody flows at transonic speeds
By James R. DeBonis
“Validation of the NPARC code for nozzle afterbody flows at transonic speeds” Metadata:
- Title: ➤ Validation of the NPARC code for nozzle afterbody flows at transonic speeds
- Author: James R. DeBonis
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Validation of the NPARC code for nozzle afterbody flows at transonic speeds” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Applications programs (Computers) - Nozzle flow - Afterbodies - Turbulence models - Program verification (Computers) - Transonic speed
Edition Identifiers:
- The Open Library ID: OL17791907M - OL15414431M
- Online Computer Library Center (OCLC) ID: 34041515
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 Validation of the NPARC code for nozzle afterbody flows at transonic speeds at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
8Effects of upper-surface nacelles on longitudinal aerodynamic characteristics of high-wing transport configuration
By Lawrence E. Putnam
“Effects of upper-surface nacelles on longitudinal aerodynamic characteristics of high-wing transport configuration” Metadata:
- Title: ➤ Effects of upper-surface nacelles on longitudinal aerodynamic characteristics of high-wing transport configuration
- Author: Lawrence E. Putnam
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1986
- Publish Location: ➤ [Washington, D.C.] - Springfield, Va
“Effects of upper-surface nacelles on longitudinal aerodynamic characteristics of high-wing transport configuration” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Airplanes - Body-wing configurations - Design and construction - Longitudinal Stability of airplanes - Nacelles - Stability of airplanes, Longitudinal - Transonic speed - Transport aircraft - Transport planes - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL16116642M - OL18218653M
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 Effects of upper-surface nacelles on longitudinal aerodynamic characteristics of high-wing transport configuration at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
9The use of hot-film technique for boundary layer studies on a 21% thick airfoil
By M. Khalid
“The use of hot-film technique for boundary layer studies on a 21% thick airfoil” Metadata:
- Title: ➤ The use of hot-film technique for boundary layer studies on a 21% thick airfoil
- Author: M. Khalid
- Language: English
- Number of Pages: Median: 46
- Publisher: ➤ NationalResearch Council Canada - National Aeronautical Establishment
- Publish Date: 1987
- Publish Location: Ottawa
“The use of hot-film technique for boundary layer studies on a 21% thick airfoil” Subjects and Themes:
- Subjects: Hot-film anemometers - Boundary layer flow - Airfoils - Transonic speed
Edition Identifiers:
- The Open Library ID: OL13909883M - OL19246563M
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 The use of hot-film technique for boundary layer studies on a 21% thick airfoil at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
10Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method
By Euromech Colloquium (349th 1996 Göttingen, Germany)
“Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method” Metadata:
- Title: ➤ Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method
- Author: ➤ Euromech Colloquium (349th 1996 Göttingen, Germany)
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method” Subjects and Themes:
- Subjects: ➤ Airfoil oscillations - Airfoils - Boundary layer separation - Computational fluid dynamics - Coupling - Mach number - Separated flow - Transonic flow - Transonic flutter - Transonic speed - Unsteady flow - Viscous flow
Edition Identifiers:
- The Open Library ID: OL17595884M - OL15518388M
- Online Computer Library Center (OCLC) ID: 42671384
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 Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
11Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds
By John E. Lamar
“Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds” Metadata:
- Title: ➤ Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds
- Author: John E. Lamar
- Language: English
- Publisher: ➤ Available from NASA Center for AeroSpace Information (CASI) - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 2001
- Publish Location: Hanover MD - Hampton, Va
“Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds” Subjects and Themes:
- Subjects: ➤ Aerodynamics - Aerodynamic characteristics - Computational fluid dynamics - Subsonic speed - Transonic speed - Wind tunnel tests - Wing profiles - Geometry - Flight tests - Data integration
Edition Identifiers:
- The Open Library ID: OL17610253M
- Online Computer Library Center (OCLC) ID: 51617379
Access and General Info:
- First Year Published: 2001
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
12Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane
By Dennis O. Allison
“Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane” Metadata:
- Title: ➤ Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane
- Author: Dennis O. Allison
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service (NTIS) [distributor
- Publish Date: 1995
- Publish Location: Springfield, VA - Hampton, Va
“Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane” Subjects and Themes:
- Subjects: ➤ Pressure distribution - Wind tunnel tests - Aircraft models - Subsonic speed - Transonic speed - Maneuverability - Trailing edges - Airfoils - Wing-fuselage stores - Leading edges
Edition Identifiers:
- The Open Library ID: OL15413576M
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 Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
13Response of high subsonic jet to nonaxisymmetric disturbances
By Alvin Bayliss
“Response of high subsonic jet to nonaxisymmetric disturbances” Metadata:
- Title: ➤ Response of high subsonic jet to nonaxisymmetric disturbances
- Author: Alvin Bayliss
- Language: English
- Publisher: ➤ American Institute of Aeronautics and Astronautics - National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - Reston, VA - [Washington, DC
“Response of high subsonic jet to nonaxisymmetric disturbances” Subjects and Themes:
- Subjects: ➤ Transonic speed - Antenna radiation patterns - Cylindrical coordinates - Subsonic flow - Gas jets - Flow distribution
Edition Identifiers:
- The Open Library ID: OL15509220M
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 Response of high subsonic jet to nonaxisymmetric disturbances at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
14Transonic aeroelastic analysis of launch vehicle configurations
By Joao Luiz Filgueiras de Azevedo
“Transonic aeroelastic analysis of launch vehicle configurations” Metadata:
- Title: ➤ Transonic aeroelastic analysis of launch vehicle configurations
- Author: ➤ Joao Luiz Filgueiras de Azevedo
- Number of Pages: Median: 154
- Publisher: Langley Research Center
- Publish Date: 1988
- Publish Location: Hampton, Va
“Transonic aeroelastic analysis of launch vehicle configurations” Subjects and Themes:
- Subjects: Aeroelasticity - Launch vehicle configurations - Transonic speed
Edition Identifiers:
- The Open Library ID: OL18928873M
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 Transonic aeroelastic analysis of launch vehicle configurations at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
15Flow unsteadiness effects on boundary layers
By Sreedhara V. Murthy
“Flow unsteadiness effects on boundary layers” Metadata:
- Title: ➤ Flow unsteadiness effects on boundary layers
- Author: Sreedhara V. Murthy
- Language: English
- Publisher: NASA Ames Research Center
- Publish Date: 1989
- Publish Location: [Moffett Field, Calif
“Flow unsteadiness effects on boundary layers” Subjects and Themes:
- Subjects: ➤ Boundary layer transition - Boundary layers - Data bases - Databases - Subsonic speed - Transonic speed - Wind tunnel calibration - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL16125542M
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 Flow unsteadiness effects on boundary layers at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
16Flight demonstration of a shock location sensor using constant voltage hot-film anemometry
By Timothy R. Moes
“Flight demonstration of a shock location sensor using constant voltage hot-film anemometry” Metadata:
- Title: ➤ Flight demonstration of a shock location sensor using constant voltage hot-film anemometry
- Author: Timothy R. Moes
- Language: English
- Publisher: ➤ National Technical Information Service, distributor] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1997
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va
“Flight demonstration of a shock location sensor using constant voltage hot-film anemometry” Subjects and Themes:
- Subjects: ➤ F-15 aircraft - Hot-film anemometers - Airfoils - Laminar boundary layer - Leading edges - Pressure sensors - Transonic speed
Edition Identifiers:
- The Open Library ID: OL15504664M
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 Flight demonstration of a shock location sensor using constant voltage hot-film anemometry at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
17PARC3D calculations of the F/A-18A HARV inlet vortex generators
By Steve D. Podleski
“PARC3D calculations of the F/A-18A HARV inlet vortex generators” Metadata:
- Title: ➤ PARC3D calculations of the F/A-18A HARV inlet vortex generators
- Author: Steve D. Podleski
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“PARC3D calculations of the F/A-18A HARV inlet vortex generators” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Flow distortion - F-18 aircraft - Separated flow - Computational grids - Vortex generators - Applications programs (Computers) - Transonic speed - Engine inlets - Maneuverability - Research vehicles
Edition Identifiers:
- The Open Library ID: OL15425817M
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 PARC3D calculations of the F/A-18A HARV inlet vortex generators at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
18Comparison of the aerodynamic characteristics of similar models in two size wind tunnels at transonic speeds
By A. M. Springer
“Comparison of the aerodynamic characteristics of similar models in two size wind tunnels at transonic speeds” Metadata:
- Title: ➤ Comparison of the aerodynamic characteristics of similar models in two size wind tunnels at transonic speeds
- Author: A. M. Springer
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1998
- Publish Location: ➤ Springfield, Va - [Washington, D.C
“Comparison of the aerodynamic characteristics of similar models in two size wind tunnels at transonic speeds” Subjects and Themes:
- Subjects: Wind tunnel models - Transonic speed - Scale models - Aerodynamic characteristics
Edition Identifiers:
- The Open Library ID: OL15546876M
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 Comparison of the aerodynamic characteristics of similar models in two size wind tunnels at transonic speeds at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
19Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept
By A. M. Springer
“Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept” Metadata:
- Title: ➤ Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept
- Author: A. M. Springer
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Marshall Space Flight Center
- Publish Date: 1995
- Publish Location: [Springfield, Va - MSFC, Ala
“Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept” Subjects and Themes:
- Subjects: ➤ Body-wing configurations - Aerodynamic characteristics - Wind tunnel tests - Longitudinal stability - Subsonic speed - Aerodynamic stability - Angle of attack - Single stage to orbit vehicles - Sideslip - Aerodynamic forces - Lateral stability - Control surfaces - Transonic speed - Mach number - Spacecraft stability
Edition Identifiers:
- The Open Library ID: OL15416729M
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 Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
20Final report on investigation of transonic flow over segmented slotted wind tunnel wall with mass transfer
By M. K. Bhat
“Final report on investigation of transonic flow over segmented slotted wind tunnel wall with mass transfer” Metadata:
- Title: ➤ Final report on investigation of transonic flow over segmented slotted wind tunnel wall with mass transfer
- Author: M. K. Bhat
- Language: English
- Publisher: ➤ NASA Ames Research Center - The University of Tennessee Space Institute - For sale by the National Technical Information Service
- Publish Date: 1990
- Publish Location: ➤ [Springfield, VA - Tullahoma, TN - [Moffett Field, CA]
“Final report on investigation of transonic flow over segmented slotted wind tunnel wall with mass transfer” Subjects and Themes:
- Subjects: ➤ Boundary layers - Flow velocity - Vibration - Transonic flow - Slotted wind tunnels - Flow distribution - Suction - Transonic speed - Mass transfer - Wind tunnel walls
Edition Identifiers:
- The Open Library ID: OL16129990M
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 Final report on investigation of transonic flow over segmented slotted wind tunnel wall with mass transfer at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
21Preliminary testing of a twisted Delta propeller for transonic cruise speed
By Malcolm D. Imray
“Preliminary testing of a twisted Delta propeller for transonic cruise speed” Metadata:
- Title: ➤ Preliminary testing of a twisted Delta propeller for transonic cruise speed
- Author: Malcolm D. Imray
- Publisher: ➤ Carleton University, Department of Mechanical and Aeronautical Engineering
- Publish Date: 1986
- Publish Location: Ottawa, Ontario
“Preliminary testing of a twisted Delta propeller for transonic cruise speed” Subjects and Themes:
- Subjects: Propellers - Transonic speed
Edition Identifiers:
- The Open Library ID: OL19004781M
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 Preliminary testing of a twisted Delta propeller for transonic cruise speed at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.