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Source: The Open Library
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1Subsonic-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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2Skin-friction measurements in a 3-D, supersonic shock-wave/boundary-layer interaction
By Aerospace Sciences Meeting & Exhibit (32nd 1994 Reno, Nev.)
“Skin-friction measurements in a 3-D, supersonic shock-wave/boundary-layer interaction” Metadata:
- Title: ➤ Skin-friction measurements in a 3-D, supersonic shock-wave/boundary-layer interaction
- Author: ➤ Aerospace Sciences Meeting & Exhibit (32nd 1994 Reno, Nev.)
- Language: English
- Publisher: ➤ American Institute of Aeronautics and Astronautics - [National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ Springfield, Va - Washington, D.C
“Skin-friction measurements in a 3-D, supersonic shock-wave/boundary-layer interaction” Subjects and Themes:
- Subjects: Boundary layers - Free flow - Skin friction - Supersonic speed - Turbulence models
Edition Identifiers:
- The Open Library ID: OL17135643M - OL18138002M - OL17593576M - OL15557726M
- Online Computer Library Center (OCLC) ID: 42817199
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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3Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel
By Richard J. Re
“Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel” Metadata:
- Title: ➤ Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel
- Author: Richard J. Re
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1998
- Publish Location: Hampton, Va - [Springfield, Va
“Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel” Subjects and Themes:
- Subjects: ➤ Static pressure - Supersonic speed - Bow waves - Bodies of revolution - Mach number - Supersonic transports - Shock waves
Edition Identifiers:
- The Open Library ID: OL17582810M - OL17131907M - OL18134345M - OL15546619M
- Online Computer Library Center (OCLC) ID: 41598366
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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4Navier-Stokes simulation of several high-lift reference H configurations
By Wendy B. Lessard
“Navier-Stokes simulation of several high-lift reference H configurations” Metadata:
- Title: ➤ Navier-Stokes simulation of several high-lift reference H configurations
- Author: Wendy B. Lessard
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service [distributor - Available from NASA Center for AeroSpace Information
- Publish Date: 1999
- Publish Location: ➤ Springfield, VA - Hampton, Va - Hanover, MD
“Navier-Stokes simulation of several high-lift reference H configurations” Subjects and Themes:
- Subjects: ➤ Aerodynamic configurations - Angle of attack - Body-wing configurations - Computational fluid dynamics - Navier-Stokes equation - Reynolds number - Structured grids (Mathematics) - Supersonic speed - Supersonic transports - Vortices - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL15569338M - OL18140130M - OL18296120M - OL17595527M
- Online Computer Library Center (OCLC) ID: 44441535
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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5Preliminary airborne measurements for the SR-71 sonic boom propagation experiment
By Edward A. Haering
“Preliminary airborne measurements for the SR-71 sonic boom propagation experiment” Metadata:
- Title: ➤ Preliminary airborne measurements for the SR-71 sonic boom propagation experiment
- Author: Edward A. Haering
- Language: English
- Publisher: ➤ National Technical Information Service, distributor] - National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - Edwards, Calif
“Preliminary airborne measurements for the SR-71 sonic boom propagation experiment” Subjects and Themes:
- Subjects: ➤ Pressure measurement - Supersonic speed - SR-71 aircraft - Flight altitude - Sonic booms - Mach number - Weight (Mass) - Flight tests
Edition Identifiers:
- The Open Library ID: OL15421592M - OL17796148M
- Online Computer Library Center (OCLC) ID: 35205991
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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6First order ozone impact of a fleet of supersonic business jets (SSBJs)
By Steven L. Baughcum
“First order ozone impact of a fleet of supersonic business jets (SSBJs)” Metadata:
- Title: ➤ First order ozone impact of a fleet of supersonic business jets (SSBJs)
- Author: Steven L. Baughcum
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Glenn Research Center - Available from NASA Center for Aerospace Information
- Publish Date: 2002
- Publish Location: ➤ Hanover, MD - [Cleveland, Ohio]
“First order ozone impact of a fleet of supersonic business jets (SSBJs)” Subjects and Themes:
- Subjects: ➤ Civil aviation - Contaminants - Exhaust emission - Ozonosphere - Supersonc transports - Supersonic speed
Edition Identifiers:
- The Open Library ID: OL16056858M - OL17620424M
- Online Computer Library Center (OCLC) ID: 53039302
Access and General Info:
- First Year Published: 2002
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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7Numerical 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
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8Inviscid 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
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9Evaluation of an ejector ramjet based propulsion system for air-breathing hypersonic flight
By Scott R. Thomas
“Evaluation of an ejector ramjet based propulsion system for air-breathing hypersonic flight” Metadata:
- Title: ➤ Evaluation of an ejector ramjet based propulsion system for air-breathing hypersonic flight
- Author: Scott R. Thomas
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Evaluation of an ejector ramjet based propulsion system for air-breathing hypersonic flight” Subjects and Themes:
- Subjects: ➤ Hydrocarbon fuels - Supersonic speed - Propulsion system performance - Flow distribution - Engine tests - Integral rocket ramjets - Mach number - Ejectors - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL15484276M - OL17822489M
- Online Computer Library Center (OCLC) ID: 38850490
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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10Flow coefficient behavior for boundary layer bleed holes and slots
By B. P. Willis
“Flow coefficient behavior for boundary layer bleed holes and slots” Metadata:
- Title: ➤ Flow coefficient behavior for boundary layer bleed holes and slots
- Author: B. P. Willis
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Flow coefficient behavior for boundary layer bleed holes and slots” Subjects and Themes:
- Subjects: ➤ Boundary layter control - Wind tunnel tests - Supersonic speed - Flow coefficients - Mach number - Orifices
Edition Identifiers:
- The Open Library ID: OL17788783M - OL15411107M
- Online Computer Library Center (OCLC) ID: 32869533
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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11Lee-side flow over delta wings at supersonic speeds
By David S. Miller
“Lee-side flow over delta wings at supersonic speeds” Metadata:
- Title: ➤ Lee-side flow over delta wings at supersonic speeds
- Author: David S. Miller
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service
- Publish Date: 1985
- Publish Location: ➤ [Washington, D.C.] - Springfield, Va
“Lee-side flow over delta wings at supersonic speeds” Subjects and Themes:
- Subjects: Delta wings - Supersonic speed - Leading edges - Flow visualization - Vortices
Edition Identifiers:
- The Open Library ID: OL18217697M - OL16114989M
Access and General Info:
- First Year Published: 1985
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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12High speed nozzles task
By A. Hamed
“High speed nozzles task” Metadata:
- Title: High speed nozzles task
- Author: A. Hamed
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - University of Cincinnati - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Cincinnati, Ohio?] - [Washington, DC
“High speed nozzles task” Subjects and Themes:
- Subjects: ➤ Convergent-divergent nozzles - Exhaust nozzles - Nozzle design - Nozzle flow - Pressure ratio - Supersonic speed - Turbulence models
Edition Identifiers:
- The Open Library ID: OL15418953M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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13Lee-side flow over delta wings at supersonic speeds
By D. S. Miller
“Lee-side flow over delta wings at supersonic speeds” Metadata:
- Title: ➤ Lee-side flow over delta wings at supersonic speeds
- Author: D. S. Miller
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1985
- Publish Location: ➤ [Washington, D.C.] - Springfield, Va
“Lee-side flow over delta wings at supersonic speeds” Subjects and Themes:
- Subjects: Delta wings - Flow visualization - Leading edges - Supersonic speed - Vortices
Edition Identifiers:
- The Open Library ID: OL18468528M
Access and General Info:
- First Year Published: 1985
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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14High speed commercial transport fuels considerations and research needs
By C. M. Lee
“High speed commercial transport fuels considerations and research needs” Metadata:
- Title: ➤ High speed commercial transport fuels considerations and research needs
- Author: C. M. Lee
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - For sale by the National Technical Information Service
- Publish Date: 1990
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“High speed commercial transport fuels considerations and research needs” Subjects and Themes:
- Subjects: ➤ Airplanes - Fuel - Fuel combustion - Liquified gases - Methane - Supersonic speed - Thermal stability - Transport aircraft
Edition Identifiers:
- The Open Library ID: OL16128013M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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15Concept development of a Mach 2.4 high-speed civil transport
“Concept development of a Mach 2.4 high-speed civil transport” Metadata:
- Title: ➤ Concept development of a Mach 2.4 high-speed civil transport
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1999
- Publish Location: [Springfield, Va - Hampton, Va
“Concept development of a Mach 2.4 high-speed civil transport” Subjects and Themes:
- Subjects: ➤ Supersonic speed - High speed - Supersonic cruise aircraft research - Supersonic transports - Supersonic aircraft - Transport aircraft - Aircraft design
Edition Identifiers:
- The Open Library ID: OL15569353M
- Online Computer Library Center (OCLC) ID: 44447753
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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16Parametric study on laminar flow for finite wings at supersonic speeds
By Joseph Avila Garcia
“Parametric study on laminar flow for finite wings at supersonic speeds” Metadata:
- Title: ➤ Parametric study on laminar flow for finite wings at supersonic speeds
- Author: Joseph Avila Garcia
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Parametric study on laminar flow for finite wings at supersonic speeds” Subjects and Themes:
- Subjects: ➤ Laminar boundary layer - Boundary layer control - Boundary layer stability - Supersonic speed - Wings - Laminar flow
Edition Identifiers:
- The Open Library ID: OL15412001M
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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17Preliminary measurement of the noise from the 2/9 scale model of the large-scale advanced propfan (LAP) propeller, SR-7A
By James H. Dittmar
“Preliminary measurement of the noise from the 2/9 scale model of the large-scale advanced propfan (LAP) propeller, SR-7A” Metadata:
- Title: ➤ Preliminary measurement of the noise from the 2/9 scale model of the large-scale advanced propfan (LAP) propeller, SR-7A
- Author: James H. Dittmar
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Lewis Research Center
- Publish Date: 1985
- Publish Location: [Cleveland, Ohio
“Preliminary measurement of the noise from the 2/9 scale model of the large-scale advanced propfan (LAP) propeller, SR-7A” Subjects and Themes:
- Subjects: ➤ Airplanes - Design analysis - Evaluation - Helical flow - Mach number - Measurement - Noise - Noise (Sound) - Noise reduction - Predictions - Prop-fan technology - Propeller blades - Scale models - Supersonic speed - Tip speed - Turbine-propeller engines - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL16151292M
Access and General Info:
- First Year Published: 1985
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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18Control effectiveness and tip-fin dihedral effects for the HL-20 lifting-body configuration at Mach numbers from 1.6 to 4.5
By Christopher I. Cruz
“Control effectiveness and tip-fin dihedral effects for the HL-20 lifting-body configuration at Mach numbers from 1.6 to 4.5” Metadata:
- Title: ➤ Control effectiveness and tip-fin dihedral effects for the HL-20 lifting-body configuration at Mach numbers from 1.6 to 4.5
- Author: Christopher I. Cruz
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service [distributor
- Publish Date: 1995
- Publish Location: ➤ Hampton, Va - NASA Center for AeroSpace Information [distributor] - Linthicum Heights, MD - Springfield, VA
“Control effectiveness and tip-fin dihedral effects for the HL-20 lifting-body configuration at Mach numbers from 1.6 to 4.5” Subjects and Themes:
- Subjects: ➤ Lifting bodies - Controllability - Dihedral angle - Supersonic speed - Mach number fins - Wind tunnel tests - Deflection
Edition Identifiers:
- The Open Library ID: OL15423225M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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19Simulation of crossflow instability on a supersonic highly swept wing
By C. David Pruett
“Simulation of crossflow instability on a supersonic highly swept wing” Metadata:
- Title: ➤ Simulation of crossflow instability on a supersonic highly swept wing
- Author: C. David Pruett
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: Hampton, Va - [Springfield, Va
“Simulation of crossflow instability on a supersonic highly swept wing” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Civil aviation - Three dimensional boundary layer - Cross flow - Flow stability - Runge-Kutta method - Boundary layer transition - Navier-Stokes equation - Incompressible flow - Supersonic speed - Supersonic transports
Edition Identifiers:
- The Open Library ID: OL15424655M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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20Effect of density gradients in confined supersonic shear layers
By Oshin Peroomian
“Effect of density gradients in confined supersonic shear layers” Metadata:
- Title: ➤ Effect of density gradients in confined supersonic shear layers
- Author: Oshin Peroomian
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Effect of density gradients in confined supersonic shear layers” Subjects and Themes:
- Subjects: ➤ Density (Mass/volume) - Supersonic combustion - Mathematical models - Cross flow - Acoustic properties - Combustion chambers - Shear layers - Modes (Standing waves) - Euler equations of motion - Vortex sheets - Three dimensional motion - Supersonic speed - Compressible flow
Edition Identifiers:
- The Open Library ID: OL15418794M
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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21Effect of milling machine roughness and wing dihedral on the supersonic aerodynamic characteristics of a highly swept wing
By Christine M. Darden
“Effect of milling machine roughness and wing dihedral on the supersonic aerodynamic characteristics of a highly swept wing” Metadata:
- Title: ➤ Effect of milling machine roughness and wing dihedral on the supersonic aerodynamic characteristics of a highly swept wing
- Author: Christine M. Darden
- Number of Pages: Median: 87
- Publisher: Langley Research Center
- Publish Date: 1989
- Publish Location: Hampton, Va
“Effect of milling machine roughness and wing dihedral on the supersonic aerodynamic characteristics of a highly swept wing” Subjects and Themes:
- Subjects: Supersonic speed - Swept wings - Surface roughness
Edition Identifiers:
- The Open Library ID: OL19379621M
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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22Effects of some geometric variations on missile aerodynamic characteristics at supersonic speeds
By M. Leroy Spearman
“Effects of some geometric variations on missile aerodynamic characteristics at supersonic speeds” Metadata:
- Title: ➤ Effects of some geometric variations on missile aerodynamic characteristics at supersonic speeds
- Author: M. Leroy Spearman
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1986
- Publish Location: Hampton, Va
“Effects of some geometric variations on missile aerodynamic characteristics at supersonic speeds” Subjects and Themes:
- Subjects: ➤ Control systems - Body-wing configurations - Guided missiles - Aerodynamics - Supersonic speed - Aerodynamic characteristics - Missile configurations - Wing span - Wing planforms
Edition Identifiers:
- The Open Library ID: OL16152761M
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.
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23Computations of axisymmetric flows in hypersonic shock tubes
By Surendra P. Sharma
“Computations of axisymmetric flows in hypersonic shock tubes” Metadata:
- Title: ➤ Computations of axisymmetric flows in hypersonic shock tubes
- Author: Surendra P. Sharma
- Language: English
- Publisher: ➤ American Institute of Aeronautics and Astronautics - National Technical Information Service, distributor - [National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - Washington, DC
“Computations of axisymmetric flows in hypersonic shock tubes” Subjects and Themes:
- Subjects: Computational fluid dynamics - Axisymmetric flow - Flow distribution - Supersonic speed - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: OL15539928M
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.
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24Experimental study at low supersonic speeds of a missile concept having opposing wraparound tails
By Jerry M. Allen
“Experimental study at low supersonic speeds of a missile concept having opposing wraparound tails” Metadata:
- Title: ➤ Experimental study at low supersonic speeds of a missile concept having opposing wraparound tails
- Author: Jerry M. Allen
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: [Springfield, Va - Hampton, Va
“Experimental study at low supersonic speeds of a missile concept having opposing wraparound tails” Subjects and Themes:
- Subjects: ➤ Canard configurations - Missile configurations - Missile control - Rolling moments - Supersonic speed - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL15408442M
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.
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25Nonlinear 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.
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Wiki
Source: Wikipedia
Wikipedia Results
Search Results from Wikipedia
Supersonic speed
Supersonic speed is the speed of an object that exceeds the speed of sound (Mach 1). For objects traveling in dry air of a temperature of 20 °C (68 °F)
Supersonic aircraft
A supersonic aircraft is an aircraft capable of supersonic flight, that is, flying faster than the speed of sound (Mach 1). Supersonic aircraft were developed
Supersonic transport
A supersonic transport (SST) or a supersonic airliner is a civilian supersonic aircraft designed to transport passengers at speeds greater than the speed
Sonic boom
emanating from the supersonic object. Rather, the boom is a continuous effect that occurs while the object is traveling at supersonic speeds and affects only
Mach number
the speed of sound. At Mach 0.65, u is 65% of the speed of sound (subsonic), and, at Mach 1.35, u is 35% faster than the speed of sound (supersonic). The
Supercruise
afterburners. Aircraft such as the SR-71 Blackbird are designed to cruise at supersonic speed with afterburners enabled. Some fighter jets are capable of supercruise
Delta wing
Jet Age, when it proved suitable for high-speed subsonic and supersonic flight. At the other end of the speed scale, the Rogallo flexible wing proved a
Hypersonic speed
[citation needed] Although "subsonic" and "supersonic" usually refer to speeds below and above the local speed of sound respectively, aerodynamicists often
Concorde
variable engine intake ramps, and reheat for take-off and acceleration to supersonic speed. Constructed from aluminium, it was the first airliner to have analogue
Scramjet
A scramjet (supersonic combustion ramjet) is a variant of a ramjet airbreathing jet engine in which combustion takes place in supersonic airflow. As in