Explore: Hypersonics
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Books Results
Source: The Open Library
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Search results from The Open Library
1The X-33 extended flight test range
By Dale A. Mackall
“The X-33 extended flight test range” Metadata:
- Title: ➤ The X-33 extended flight test range
- Author: Dale A. Mackall
- Language: English
- Number of Pages: Median: 11
- Publisher: ➤ National Technical Information Service, distributor - Available from National Technical Information Service - National Aeronautics and Space Administration, Dryden Flight Research Center
- Publish Date: 1998
- Publish Location: ➤ [Springfield, Va - Springfield, Va - Edwards, Calif
“The X-33 extended flight test range” Subjects and Themes:
- Subjects: ➤ Communication - Hypersonics - Recoverable launch vehicles - X-33 reusable launch vehicle - Plasma frequencies - Reusable launch vehicles - Flight tests - Testing - Airplanes - Handling characteristics - Flight testing - Reusable space vehicles - Launch vehicles (Astronautics)
Edition Identifiers:
- The Open Library ID: OL15542062M - OL18132752M - OL19788313M - OL17130366M - OL17580155M
- Online Computer Library Center (OCLC) ID: 41227068
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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2Development of the X-33 aerodynamic uncertainty model
By Brent R. Cobleigh
“Development of the X-33 aerodynamic uncertainty model” Metadata:
- Title: ➤ Development of the X-33 aerodynamic uncertainty model
- Author: Brent R. Cobleigh
- Language: English
- Number of Pages: Median: 33
- Publisher: ➤ National Technical Information Service, distributor - Dryden Flight Research Center - Distributed by the National Aeronautics and Space Administration] - National Aeronautics and Space Administration, Dryden Flight Research Center
- Publish Date: 1998
- Publish Location: ➤ Edwards, Calif - [Washington, D.C - [Springfield, Va
“Development of the X-33 aerodynamic uncertainty model” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Aerodynamics - Design and construction - Flight control - Hypersonics - Launch vehicles (Astronautics) - Lifting bodies - Mathematical models - Monte Carlo method - Reusable space vehicles - Space shuttle orbiters - X-33 reusable launch vehicle
Edition Identifiers:
- The Open Library ID: OL17135415M - OL19395543M - OL17701288M - OL18134932M - OL17591854M
- Online Computer Library Center (OCLC) ID: 42758571
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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3Subsonic-to-hypersonic aerodynamic characteristics for a winged, circular-body, single-stage-to-orbit spacecraft configuration
By W. Pelham Phillips
“Subsonic-to-hypersonic aerodynamic characteristics for a winged, circular-body, single-stage-to-orbit spacecraft configuration” Metadata:
- Title: ➤ Subsonic-to-hypersonic aerodynamic characteristics for a winged, circular-body, single-stage-to-orbit spacecraft configuration
- Author: W. Pelham Phillips
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Subsonic-to-hypersonic aerodynamic characteristics for a winged, circular-body, single-stage-to-orbit spacecraft configuration” Subjects and Themes:
- Subjects: ➤ Spacecraft configurations - Controllability - Supersonic speed - Subsonic speed - Aerodynamic characteristics - Single stage to orbit vehicles - Longitudinal stability - Hypersonics
Edition Identifiers:
- The Open Library ID: OL17516416M - OL17121322M - OL18100856M - OL17687502M
- Online Computer Library Center (OCLC) ID: 38290177
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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4Hypersonic 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
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5Aeroheating predictions for X-34 using an inviscid-boundary layer method
By Christopher J. Riley
“Aeroheating predictions for X-34 using an inviscid-boundary layer method” Metadata:
- Title: ➤ Aeroheating predictions for X-34 using an inviscid-boundary layer method
- Author: Christopher J. Riley
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor - National Aeronautics and Space Administration - American Institute of Aeronautics and Astronautics
- Publish Date: 1998
- Publish Location: ➤ Hampton, Va - [Washington, D.C - Springfield, Va - [Springfield, Va - Reston, VA
“Aeroheating predictions for X-34 using an inviscid-boundary layer method” Subjects and Themes:
- Subjects: ➤ Convective heat transfer - X-34 reusable launch vehicle - Boundary layers - Algorithms - Aerodynamic heating - Inviscid flow - Turbulent flow - Surface temperature - Mathematical models - Hypersonics
Edition Identifiers:
- The Open Library ID: OL17593122M - OL17838334M - OL17700851M - OL15539932M
- Online Computer Library Center (OCLC) ID: 40763813 - 42677791
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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6CFD for hypersonic propulsion
By Louis A. Povinelli
“CFD for hypersonic propulsion” Metadata:
- Title: CFD for hypersonic propulsion
- Author: Louis A. Povinelli
- Language: English
- Publisher: Lewis Research Center
- Publish Date: 1991
- Publish Location: [Cleveland, Ohio
“CFD for hypersonic propulsion” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Viscous flow - Airframes - Hypersonics - Three dimensional flow - Hypersonic flight - Propulsion system configurations - Air breathing engines - Nozzle flow - Flow distribution - Propulsion system performance
Edition Identifiers:
- The Open Library ID: OL17725560M - OL17634717M
- Online Computer Library Center (OCLC) ID: 62207170
Access and General Info:
- First Year Published: 1991
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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7Demonstration of oblique detonation wave for hypersonic propulsion
By Takashi Nakamura
“Demonstration of oblique detonation wave for hypersonic propulsion” Metadata:
- Title: ➤ Demonstration of oblique detonation wave for hypersonic propulsion
- Author: Takashi Nakamura
- Number of Pages: Median: 118
- Publisher: ➤ Astron Research and Engineering
- Publish Date: 1989
- Publish Location: Sunnyvale, Calif
“Demonstration of oblique detonation wave for hypersonic propulsion” Subjects and Themes:
- Subjects: Detonation waves - Hypersonics - Hypervelocity launchers
Edition Identifiers:
- The Open Library ID: OL19380266M
Access and General Info:
- First Year Published: 1989
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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8Hypersonic boundary-layer transition for X-33 phase II vehicle
By R. A. Thompson
“Hypersonic boundary-layer transition for X-33 phase II vehicle” Metadata:
- Title: ➤ Hypersonic boundary-layer transition for X-33 phase II vehicle
- Author: R. A. Thompson
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - American Institute of Aeronautics and Astronautics - National Aeronautics and Space Administration
- Publish Date: 1998
- Publish Location: ➤ Reston, Va - [Washington, DC - Springfield, Va
“Hypersonic boundary-layer transition for X-33 phase II vehicle” Subjects and Themes:
- Subjects: ➤ Flow visualization - Boundary layer transition - Hypersonics - Finite volume method - Wind tunnel tests - Flow distribution
Edition Identifiers:
- The Open Library ID: OL17578604M
- Online Computer Library Center (OCLC) ID: 40771865
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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9Summary of shock tunnel development and application to hypersonic research
By Abraham Hertzberg
“Summary of shock tunnel development and application to hypersonic research” Metadata:
- Title: ➤ Summary of shock tunnel development and application to hypersonic research
- Author: Abraham Hertzberg
- Number of Pages: Median: 97
- Publisher: ➤ Cornell Aeronautical Laboratory
- Publish Date: 1961
- Publish Location: Buffalo, N. Y
“Summary of shock tunnel development and application to hypersonic research” Subjects and Themes:
- Subjects: Hypersonics - Hypersonic shock tubes
Edition Identifiers:
- The Open Library ID: OL19246005M
Access and General Info:
- First Year Published: 1961
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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10Hypersonic turbulent boundary-layer and free shear database
By Gary S. Settles
“Hypersonic turbulent boundary-layer and free shear database” Metadata:
- Title: ➤ Hypersonic turbulent boundary-layer and free shear database
- Author: Gary S. Settles
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ Moffett Field, Calif - [Springfield, Va
“Hypersonic turbulent boundary-layer and free shear database” Subjects and Themes:
- Subjects: ➤ Data bases - Databases - Hypersonic boundary layer - Hypersonics - Shear layers - Turbulence - Turbulence models - Turbulent boundary layer - Turbulent mixing
Edition Identifiers:
- The Open Library ID: OL15403294M
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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11The kinetic nonequilibrium processes in the internal flow and in the plume of subsonic and supersonic aircrafts
By Alexander M. Starik
“The kinetic nonequilibrium processes in the internal flow and in the plume of subsonic and supersonic aircrafts” Metadata:
- Title: ➤ The kinetic nonequilibrium processes in the internal flow and in the plume of subsonic and supersonic aircrafts
- Author: Alexander M. Starik
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, DC
“The kinetic nonequilibrium processes in the internal flow and in the plume of subsonic and supersonic aircrafts” Subjects and Themes:
- Subjects: ➤ Supersonic aircraft - Internal flow - Plumes - Hypersonics - Kinetics - Nonequilibrium conditions
Edition Identifiers:
- The Open Library ID: OL15543552M
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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12An approximate Riemann solver for thermal and chemical nonequilibrium flows
By Ramadas K. Prabhu
“An approximate Riemann solver for thermal and chemical nonequilibrium flows” Metadata:
- Title: ➤ An approximate Riemann solver for thermal and chemical nonequilibrium flows
- Author: Ramadas K. Prabhu
- 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
“An approximate Riemann solver for thermal and chemical nonequilibrium flows” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Inviscid flow - Aerothermodynamics - Nonequilibrium flow - Gas flow - Hypersonics
Edition Identifiers:
- The Open Library ID: OL15409797M
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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13Internal performance predictions for Langley scramjet engine module
By S. Z. Pinckney
“Internal performance predictions for Langley scramjet engine module” Metadata:
- Title: ➤ Internal performance predictions for Langley scramjet engine module
- Author: S. Z. Pinckney
- Number of Pages: Median: 81
- Publisher: Langley Research Center
- Publish Date: 1978
- Publish Location: Hampton, Va
“Internal performance predictions for Langley scramjet engine module” Subjects and Themes:
- Subjects: ➤ Hypersonics - Supersonic combustion ramjet engine
Edition Identifiers:
- The Open Library ID: OL19986073M
Access and General Info:
- First Year Published: 1978
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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14A dynamic response model for pressure sensors in continuum and high Knudsen number flows with large temperature gradients
By Stephen A. Whitmore
“A dynamic response model for pressure sensors in continuum and high Knudsen number flows with large temperature gradients” Metadata:
- Title: ➤ A dynamic response model for pressure sensors in continuum and high Knudsen number flows with large temperature gradients
- Author: Stephen A. Whitmore
- Language: English
- Publisher: ➤ National Technical Information Service, distributor] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1996
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“A dynamic response model for pressure sensors in continuum and high Knudsen number flows with large temperature gradients” Subjects and Themes:
- Subjects: ➤ Rarefied gas dynamics - Dynamic models - Knudsen flow - Hypersonics - Pressure sensors - Continuum flow - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: OL15423231M
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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15Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0
By Ira J. Walker
“Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0” Metadata:
- Title: ➤ Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0
- Author: Ira J. Walker
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program - National Technical Information Service, distributor]
- Publish Date: 1993
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0” Subjects and Themes:
- Subjects: ➤ Stabilizers (Fluid dynamics) - Canard configurations - Hypersonics - Aerodynamic characteristics - Delta wings - Wind tunnel tests - Research vehicles - Mach number - Hypersonic vehicles - Tail assemblies
Edition Identifiers:
- The Open Library ID: OL15403234M
Access and General Info:
- First Year Published: 1993
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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16Thermal and structural assessments of a ceramic wafer seal in hypersonic engines
By Michael T. Tong
“Thermal and structural assessments of a ceramic wafer seal in hypersonic engines” Metadata:
- Title: ➤ Thermal and structural assessments of a ceramic wafer seal in hypersonic engines
- Author: Michael T. Tong
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - For sale by the National Technical Information Service
- Publish Date: 1991
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Thermal and structural assessments of a ceramic wafer seal in hypersonic engines” Subjects and Themes:
- Subjects: ➤ Structural reliability - Failure analysis - Hypersonics - Seals (Stoppers) - Finite element method - Weibull density functions - Structural analysis - Wafers - Ceramics
Edition Identifiers:
- The Open Library ID: OL15405598M
Access and General Info:
- First Year Published: 1991
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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17Airbreathing hypersonic systems focus at NASA Langley Research Center
By James L. Hunt
“Airbreathing hypersonic systems focus at NASA Langley Research Center” Metadata:
- Title: ➤ Airbreathing hypersonic systems focus at NASA Langley Research Center
- Author: James L. Hunt
- Language: English
- Publisher: ➤ [National Aeronautics and Space Administration - American Institute of Aeronautics and Astronautics - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: ➤ Washington, DC - Springfield, Va
“Airbreathing hypersonic systems focus at NASA Langley Research Center” Subjects and Themes:
- Subjects: Air breathing engines - Hypersonics - Hypersonic aircraft
Edition Identifiers:
- The Open Library ID: OL15507851M
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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18Systems challenges for hypersonic vehicles
By James L. Hunt
“Systems challenges for hypersonic vehicles” Metadata:
- Title: ➤ Systems challenges for hypersonic vehicles
- Author: James L. Hunt
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“Systems challenges for hypersonic vehicles” Subjects and Themes:
- Subjects: ➤ Air breathing engines - Hydrogen fuels - Hydrocarbon fuels - Hypersonics - Hypersonic vehicles - Rocket engines
Edition Identifiers:
- The Open Library ID: OL15498496M
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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19An outlook on hypersonic flight
By Griffin Y. Anderson
“An outlook on hypersonic flight” Metadata:
- Title: ➤ An outlook on hypersonic flight
- Author: Griffin Y. Anderson
- Publisher: AIAA
- Publish Date: 1987
- Publish Location: New York
“An outlook on hypersonic flight” Subjects and Themes:
- Subjects: ➤ Hypersonics - Supersonic combustion ramjet engines
Edition Identifiers:
- The Open Library ID: OL19250607M
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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20Inclusion of chemical kinetics into beam-warming based PNS model for hypersonic propulsion applications
By N. Sinha
“Inclusion of chemical kinetics into beam-warming based PNS model for hypersonic propulsion applications” Metadata:
- Title: ➤ Inclusion of chemical kinetics into beam-warming based PNS model for hypersonic propulsion applications
- Author: N. Sinha
- Number of Pages: Median: 13
- Publisher: AIAA
- Publish Date: 1987
- Publish Location: New York
“Inclusion of chemical kinetics into beam-warming based PNS model for hypersonic propulsion applications” Subjects and Themes:
- Subjects: Hypersonics - Reaction kinetics - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: OL19250652M
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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21Mach 6 experimental and theoretical stability and performance of a cruciform missile at angles of attack up to 65 degrees
By Edward R. Hartmann
“Mach 6 experimental and theoretical stability and performance of a cruciform missile at angles of attack up to 65 degrees” Metadata:
- Title: ➤ Mach 6 experimental and theoretical stability and performance of a cruciform missile at angles of attack up to 65 degrees
- Author: Edward R. Hartmann
- Number of Pages: Median: 38
- Publisher: Langley Research Center
- Publish Date: 1987
- Publish Location: Hampton, Va
“Mach 6 experimental and theoretical stability and performance of a cruciform missile at angles of attack up to 65 degrees” Subjects and Themes:
- Subjects: Stability - Hypersonics - Cruciform missile
Edition Identifiers:
- The Open Library ID: OL19002630M
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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22Pitot-pressure measurements in the nozzle of the UTIAS 11" x 15" hypersonic shock tunnel
By R. P. Mason
“Pitot-pressure measurements in the nozzle of the UTIAS 11" x 15" hypersonic shock tunnel” Metadata:
- Title: ➤ Pitot-pressure measurements in the nozzle of the UTIAS 11" x 15" hypersonic shock tunnel
- Author: R. P. Mason
- Number of Pages: Median: 50
- Publisher: ➤ [Institute for Aerospace Studies]
- Publish Date: 1965
- Publish Location: [Downsview, Ont.]
“Pitot-pressure measurements in the nozzle of the UTIAS 11" x 15" hypersonic shock tunnel” Subjects and Themes:
- Subjects: Hypersonics - Shock tubes
Edition Identifiers:
- The Open Library ID: OL18997852M
Access and General Info:
- First Year Published: 1965
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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23Morphology of a standing oblique detonation wave
By David T. Pratt
“Morphology of a standing oblique detonation wave” Metadata:
- Title: ➤ Morphology of a standing oblique detonation wave
- Author: David T. Pratt
- Number of Pages: Median: 10
- Publisher: AIAA
- Publish Date: 1987
- Publish Location: New York
“Morphology of a standing oblique detonation wave” Subjects and Themes:
- Subjects: Detonation waves - Hypersonics - Oblique shock waves
Edition Identifiers:
- The Open Library ID: OL19250677M
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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24An approximate axisymmetric viscous shock layer aeroheating method for three-dimensional bodies
By Irina G. Brykina
“An approximate axisymmetric viscous shock layer aeroheating method for three-dimensional bodies” Metadata:
- Title: ➤ An approximate axisymmetric viscous shock layer aeroheating method for three-dimensional bodies
- Author: Irina G. Brykina
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Lyndon B. Johnson Space Center - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: ➤ [Springfield, Va - Houston, Tex
“An approximate axisymmetric viscous shock layer aeroheating method for three-dimensional bodies” Subjects and Themes:
- Subjects: ➤ Axisymmetric flow - Blunt bodies - Axisymmetric bodies - Aerodynamic heating - Flow measurement - Hypersonics - Parabolic bodies
Edition Identifiers:
- The Open Library ID: OL15539983M
- Online Computer Library Center (OCLC) ID: 40771789
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:
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Find An approximate axisymmetric viscous shock layer aeroheating method for three-dimensional bodies at online marketplaces:
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