Explore: Mach Number
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Source: The Open Library
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Search results from The Open Library
1The quest for mach one
By Chuck Yeager
“The quest for mach one” Metadata:
- Title: The quest for mach one
- Author: Chuck Yeager
- Language: English
- Number of Pages: Median: 142
- Publisher: Penguin Studio
- Publish Date: 1997
- Publish Location: New York, N.Y
“The quest for mach one” Subjects and Themes:
- Subjects: ➤ Test pilots - Supersonic Aerodynamics - Interviews - History - Bell X-1 (Supersonic planes) - Research - Bell X-1 (Supersonic plane) - Aeronautics, history - Mach number
- Places: United States
Edition Identifiers:
- The Open Library ID: OL445689M
- Online Computer Library Center (OCLC) ID: 37815020
- Library of Congress Control Number (LCCN): 98158669
- All ISBNs: 0670874604 - 9780670874606
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: Yes
- Is The Book Public: No
- Access Status: Borrowable
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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
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3Euler/Navier-Stokes flow computations on flexible configurations for stability analysis
By G. Guruswamy
“Euler/Navier-Stokes flow computations on flexible configurations for stability analysis” Metadata:
- Title: ➤ Euler/Navier-Stokes flow computations on flexible configurations for stability analysis
- Author: G. Guruswamy
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, American Institute of Aeronautics and Astronautics
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Washington, D.C
“Euler/Navier-Stokes flow computations on flexible configurations for stability analysis” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Structured grids (Mathematics) - Turbulence models - Finite difference theory - Aerodynamic stability - Navier-Stokes equation - Longitudinal stability - Stability derivatives - Angle of attack - Mach number
Edition Identifiers:
- The Open Library ID: OL17122527M - OL15452312M - OL17573079M - OL18100861M
- Online Computer Library Center (OCLC) ID: 38733169
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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4Progress in Favré-Reynolds stress closures for compressible flows
By V. Adumitroaie
“Progress in Favré-Reynolds stress closures for compressible flows” Metadata:
- Title: ➤ Progress in Favré-Reynolds stress closures for compressible flows
- Author: V. Adumitroaie
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - Institute for Computer Applications in Science and Engineering, NASA Langley Research Center
- Publish Date: 1998
- Publish Location: Hampton, VA - Springfield, VA
“Progress in Favré-Reynolds stress closures for compressible flows” Subjects and Themes:
- Subjects: Compressible boundary layer - Reynolds stress - Mach number - Mixing layers (Fluids) - Compressible flow
Edition Identifiers:
- The Open Library ID: OL17130964M - OL18133568M - OL15545018M - OL17839065M
- Online Computer Library Center (OCLC) ID: 41358729
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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5High-resolution shock capturing scheme for high Mach number internal flow
By Seokkwan Yoon
“High-resolution shock capturing scheme for high Mach number internal flow” Metadata:
- Title: ➤ High-resolution shock capturing scheme for high Mach number internal flow
- Author: Seokkwan Yoon
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1986
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“High-resolution shock capturing scheme for high Mach number internal flow” Subjects and Themes:
- Subjects: Computational fluid dynamics - High resolution - Hypersonic flow - Mach number - Shock waves
Edition Identifiers:
- The Open Library ID: OL15416509M - OL18082805M - OL14984577M - OL18007657M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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6Near-optimal operation of dual-fuel launch vehicles
By M. Ardema
“Near-optimal operation of dual-fuel launch vehicles” Metadata:
- Title: ➤ Near-optimal operation of dual-fuel launch vehicles
- Author: M. Ardema
- Language: English
- Publisher: ➤ American Institute of Aeronautics and Astronautics - National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1996
- Publish Location: ➤ Reston, VA - [Washington, DC - Springfield, Va
“Near-optimal operation of dual-fuel launch vehicles” Subjects and Themes:
- Subjects: ➤ Guidance (Motion) - Single stage to orbit vehicles - Trajectory optimization - Propulsion system performance - Algorithms - Ascent trajectories - Mach number - Flight paths
Edition Identifiers:
- The Open Library ID: OL17837327M - OL17126502M - OL18121645M - OL15505687M
- Online Computer Library Center (OCLC) ID: 40217103
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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7Flow-separation patterns on symmetric forebodies
By Earl R. Keener
“Flow-separation patterns on symmetric forebodies” Metadata:
- Title: ➤ Flow-separation patterns on symmetric forebodies
- Author: Earl R. Keener
- Language: English
- Number of Pages: Median: 135
- Publisher: ➤ For sale by the National Technical Information Service] - Ames Research Center - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1986 - 1987
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif - [Washington, DC]
“Flow-separation patterns on symmetric forebodies” Subjects and Themes:
- Subjects: ➤ Flow visualization - Vortex shedding - Boundary layer transition - Reynolds number - Aerodynamics - Mach number - Angle of attack
Edition Identifiers:
- The Open Library ID: OL18032518M - OL17099358M - OL19985950M - OL15288167M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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8F-18 High Alpha Research Vehicle surface pressures
By David F. Fisher
“F-18 High Alpha Research Vehicle surface pressures” Metadata:
- Title: ➤ F-18 High Alpha Research Vehicle surface pressures
- Author: David F. Fisher
- Language: English
- Number of Pages: Median: 36
- Publisher: ➤ National Technical Information Service, distributor] - NASA Ames Resarch Center, Dryden Flight Research Facility
- Publish Date: 1990 - 1991
- Publish Location: ➤ [Springfield, Va - Edwards, Calif
“F-18 High Alpha Research Vehicle surface pressures” Subjects and Themes:
- Subjects: ➤ Flow visualization - Aerodynamic load - F-18 aircraft - Pressure distribution - Wind tunnel tests - Forebodies - Angle of attack - Flight tests - Leading edges - Mach number
Edition Identifiers:
- The Open Library ID: OL20571043M - OL18249920M - OL17633879M - OL16132243M
- Online Computer Library Center (OCLC) ID: 57136710
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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9Impingement 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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10User manual for NASA Lewis 10- by 10-Foot Supersonic Wind Tunnel
By Ronald H. Soeder
“User manual for NASA Lewis 10- by 10-Foot Supersonic Wind Tunnel” Metadata:
- Title: ➤ User manual for NASA Lewis 10- by 10-Foot Supersonic Wind Tunnel
- Author: Ronald H. Soeder
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1992 - 1995
- Publish Location: ➤ [Washington, DC - [Springfield, Va - [Washington, DC] - Springfield, Va
“User manual for NASA Lewis 10- by 10-Foot Supersonic Wind Tunnel” Subjects and Themes:
- Subjects: ➤ Supersonic wind tunnels - Performance tests - Dynamic pressure - User manuals (Computer programs) - Reynolds number - Wind tunnel tests - Mach number
Edition Identifiers:
- The Open Library ID: OL14687584M - OL17796406M - OL15425389M - OL17677053M
- Online Computer Library Center (OCLC) ID: 35268400
Access and General Info:
- First Year Published: 1992
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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11Hypersonic pitching-moment shift for stardust reentry capsule forebody
By William A. Wood
“Hypersonic pitching-moment shift for stardust reentry capsule forebody” Metadata:
- Title: ➤ Hypersonic pitching-moment shift for stardust reentry capsule forebody
- Author: William A. Wood
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1997
- Publish Location: Hampton, Va - Springfield, VA
“Hypersonic pitching-moment shift for stardust reentry capsule forebody” Subjects and Themes:
- Subjects: ➤ Aerodynamic coefficients - Computational fluid dynamics - Hypersonic flow - Mach number - Navier-Stokes equation - Pitching moments - Space capsules
Edition Identifiers:
- The Open Library ID: OL17582192M - OL18137055M - OL15554563M - OL17132065M
- Online Computer Library Center (OCLC) ID: 41618396
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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12Shock-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
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13Control of unsteady separated flow associated with the dynamic stall of airfoils
By Michael C. Wilder
“Control of unsteady separated flow associated with the dynamic stall of airfoils” Metadata:
- Title: ➤ Control of unsteady separated flow associated with the dynamic stall of airfoils
- Author: Michael C. Wilder
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor - MCAT Institute
- Publish Date: 1992 - 1994 - 1995
- Publish Location: ➤ Springfield, Va - [Washington, DC - Springfield, Va.? - San Jose, CA
“Control of unsteady separated flow associated with the dynamic stall of airfoils” Subjects and Themes:
- Subjects: ➤ Unsteady flow - Wind tunnel tests - Leading edges - Aerodynamic stalling - Boundary layer control - Unsteady flow (Aerodynamics) - Separated flow - Boundary layer separation - Reynolds number - Supercritical airfoils - Airfoil oscillations - Airfoil profiles - Airfoils - Mach number - Active control
Edition Identifiers:
- The Open Library ID: OL15365679M - OL15408283M - OL15415078M
Access and General Info:
- First Year Published: 1992
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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14Full flight envelope direct thrust measurement on a supersonic aircraft
By Timothy R. Conners
“Full flight envelope direct thrust measurement on a supersonic aircraft” Metadata:
- Title: ➤ Full flight envelope direct thrust measurement on a supersonic aircraft
- Author: Timothy R. Conners
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Dryden Flight Research Center
- Publish Date: 1998
- Publish Location: ➤ Edwards, Calif - [Springfield, Va
“Full flight envelope direct thrust measurement on a supersonic aircraft” Subjects and Themes:
- Subjects: F-15 aircraft - Supersonic aircraft - Mach number - Turbofan engines
Edition Identifiers:
- The Open Library ID: OL15544011M - OL17838340M
- Online Computer Library Center (OCLC) ID: 41019967
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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15Pitot-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
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16The stability of two-dimensional wakes and shear-layers at high Mach numbers
By D. T. Papageorgiou
“The stability of two-dimensional wakes and shear-layers at high Mach numbers” Metadata:
- Title: ➤ The stability of two-dimensional wakes and shear-layers at high Mach numbers
- Author: D. T. Papageorgiou
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1990
- Publish Location: Hampton, Va
“The stability of two-dimensional wakes and shear-layers at high Mach numbers” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Inviscid flow - Shear layers - Wakes - Two dimensional flow - Hypersonic flow - Laminar flow - Flow stability - High Reynolds number - Mach number
Edition Identifiers:
- The Open Library ID: OL18263144M - OL16137874M - OL17631976M
- Online Computer Library Center (OCLC) ID: 67124982
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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17Consistent initial conditions for the DNS of compressible turbulence
By J. R. Ristorcelli
“Consistent initial conditions for the DNS of compressible turbulence” Metadata:
- Title: ➤ Consistent initial conditions for the DNS of compressible turbulence
- Author: J. R. Ristorcelli
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: Hampton, VA - [Springfield, Va
“Consistent initial conditions for the DNS of compressible turbulence” Subjects and Themes:
- Subjects: Turbulent flow - Compressibility effect - Compressible flow - Computerized simulation - Mach number
Edition Identifiers:
- The Open Library ID: OL17593388M - OL17697744M - OL17126068M
- Online Computer Library Center (OCLC) ID: 40102507
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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18Flight and wind-tunnel measurements showing base drag reduction provided by a trailing disk for high Reynolds number turbulent flow for subsonic and transonic Mach numbers
By Sheryll Goecke Powers
“Flight and wind-tunnel measurements showing base drag reduction provided by a trailing disk for high Reynolds number turbulent flow for subsonic and transonic Mach numbers” Metadata:
- Title: ➤ Flight and wind-tunnel measurements showing base drag reduction provided by a trailing disk for high Reynolds number turbulent flow for subsonic and transonic Mach numbers
- Author: Sheryll Goecke Powers
- Language: English
- Number of Pages: Median: 139
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch - Dryden Flight Research Facility
- Publish Date: 1986 - 1988
- Publish Location: ➤ Edwards, Cal - [Springfield, Va - [Washington, DC]
“Flight and wind-tunnel measurements showing base drag reduction provided by a trailing disk for high Reynolds number turbulent flow for subsonic and transonic Mach numbers” Subjects and Themes:
- Subjects: ➤ Turbulent flow - Blunt bodies - Drag reduction - Trapped vortexes - Bodies of revolution - Mach number - Drag (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL15276247M - OL20985601M - OL18029606M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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19In-flight transition measurement on a 10
By David F. Fisher
“In-flight transition measurement on a 10” Metadata:
- Title: ➤ In-flight transition measurement on a 10
- Author: David F. Fisher
- Language: English
- Number of Pages: Median: 140
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
- Publish Date: 1982
- Publish Location: ➤ [Springfield, Va - Washington, D.C
“In-flight transition measurement on a 10” Subjects and Themes:
- Subjects: Boundary layer - Mach number
Edition Identifiers:
- The Open Library ID: OL15260802M - OL18023426M - OL17548948M
Access and General Info:
- First Year Published: 1982
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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20High-lift flight tunnel
By David Lofftus
“High-lift flight tunnel” Metadata:
- Title: High-lift flight tunnel
- Author: David Lofftus
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - Available from NASA Center for Aerospace Information
- Publish Date: 2000
- Publish Location: Hanover, MD - Hampton, Va
“High-lift flight tunnel” Subjects and Themes:
- Subjects: ➤ Flight tests - Ground tests - High Reynolds number - Lift - Mach number - Test facilities - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL17607425M - OL18171258M - OL16030609M
- Online Computer Library Center (OCLC) ID: 50152830
Access and General Info:
- First Year Published: 2000
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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21Numerical simulation of the generation of axisymmetric mode jet screech tones
By Hao Shen
“Numerical simulation of the generation of axisymmetric mode jet screech tones” Metadata:
- Title: ➤ Numerical simulation of the generation of axisymmetric mode jet screech tones
- Author: Hao Shen
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor - American Institute of Aeronautics and Astronautics
- Publish Date: 1998
- Publish Location: ➤ Springfield, Va - Reston, Va - [Washington, DC
“Numerical simulation of the generation of axisymmetric mode jet screech tones” Subjects and Themes:
- Subjects: ➤ Screech tones - Axial flow - Aeroacoustics - Computerized simulation - Supersonic jet flow - Numerical flow visualization - Mach number - Axial compression loads
Edition Identifiers:
- The Open Library ID: OL17583550M - OL17701237M - OL18134632M
- Online Computer Library Center (OCLC) ID: 41639807
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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22Aeroacoustics of Low Mach Number Flows
By William Devenport and Stewart Glegg
“Aeroacoustics of Low Mach Number Flows” Metadata:
- Title: ➤ Aeroacoustics of Low Mach Number Flows
- Authors: William DevenportStewart Glegg
- Language: English
- Number of Pages: Median: 552
- Publisher: ➤ Elsevier Science & Technology - Elsevier Science & Technology Books
- Publish Date: 2017 - 2023
“Aeroacoustics of Low Mach Number Flows” Subjects and Themes:
- Subjects: ➤ Wind turbines - Aeroacoustics - Mach number - Aerodynamic noise - Aerodynamics - Mathematical models - Aérodynamique - Modèles mathématiques - Aéroacoustique - Nombre de Mach - Bruit aérodynamique - SCIENCE - Acoustics & Sound
Edition Identifiers:
- The Open Library ID: OL28624958M - OL49263678M - OL34531624M
- Online Computer Library Center (OCLC) ID: 973396718
- Library of Congress Control Number (LCCN): 2016962974
- All ISBNs: ➤ 9780128096512 - 0128097930 - 0443191123 - 9780128097939 - 0128096519 - 9780443191121
Access and General Info:
- First Year Published: 2017
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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23Comparison of the aeroacoustics of two small-scale supersonic inlets
By Wing Ng
“Comparison of the aeroacoustics of two small-scale supersonic inlets” Metadata:
- Title: ➤ Comparison of the aeroacoustics of two small-scale supersonic inlets
- Author: Wing Ng
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1996
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Comparison of the aeroacoustics of two small-scale supersonic inlets” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - Aircraft engines - Engine inlets - Flow distribution - Flow measurement - Inlet flow - Mach number - Supersonic inlets
Edition Identifiers:
- The Open Library ID: OL17593732M - OL15508989M
- Online Computer Library Center (OCLC) ID: 41272155
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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24The effects of viscosity on the stability of a trailing-line vortex in compressible flow
By Jillian A. K. Stott
“The effects of viscosity on the stability of a trailing-line vortex in compressible flow” Metadata:
- Title: ➤ The effects of viscosity on the stability of a trailing-line vortex in compressible flow
- Author: Jillian A. K. Stott
- 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
“The effects of viscosity on the stability of a trailing-line vortex in compressible flow” Subjects and Themes:
- Subjects: ➤ Viscous flow - Compressible flow - Vortices - Reynolds number - Viscosity - Mach number - Flow stability
Edition Identifiers:
- The Open Library ID: OL15404287M - OL17790339M
- Online Computer Library Center (OCLC) ID: 32296404
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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25Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method
By John W. Edwards
“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: John W. Edwards
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: Hampton, Va - [Springfield, Va
“Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Flow equations - Unsteady flow - Separated flow - Transonic flow - Transonic flutter - Mach number - Unsteady aerodynamics
Edition Identifiers:
- The Open Library ID: OL17838507M - OL15503872M
- Online Computer Library Center (OCLC) ID: 40173648
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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26Preliminary 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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27Flow quality and operational enhancements in the NASA Lewis 8- by 6-Foot Supersonic Wind Tunnel
By E. Allen Arrington
“Flow quality and operational enhancements in the NASA Lewis 8- by 6-Foot Supersonic Wind Tunnel” Metadata:
- Title: ➤ Flow quality and operational enhancements in the NASA Lewis 8- by 6-Foot Supersonic Wind Tunnel
- Author: E. Allen Arrington
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Lewis Research Center
- Publish Date: 1998
- Publish Location: ➤ [Cleveland, Ohio] - [Springfield, Va
“Flow quality and operational enhancements in the NASA Lewis 8- by 6-Foot Supersonic Wind Tunnel” Subjects and Themes:
- Subjects: Calibrating - Measuring instruments - Wind tunnels - Supersonic wind tunnels - Mach number
Edition Identifiers:
- The Open Library ID: OL17839105M - OL15544613M
- Online Computer Library Center (OCLC) ID: 41374008
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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28Numerical simulation of jet aerodynamics using the three-dimensional Navier-Stokes code PAB3D
By S. Paul Pao
“Numerical simulation of jet aerodynamics using the three-dimensional Navier-Stokes code PAB3D” Metadata:
- Title: ➤ Numerical simulation of jet aerodynamics using the three-dimensional Navier-Stokes code PAB3D
- Author: S. Paul Pao
- 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
“Numerical simulation of jet aerodynamics using the three-dimensional Navier-Stokes code PAB3D” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Computational grids - Jet flow - K-epsilon turbulence model - Mach number - Navier-Stokes equation - Subsonic flow - Supersonic flow
Edition Identifiers:
- The Open Library ID: OL17838891M - OL15504438M
- Online Computer Library Center (OCLC) ID: 40386685
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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29In-flight transition measurement on a 10p0s cone at Mach numbers from 0.5 to 2.0
By David F Fisher
“In-flight transition measurement on a 10p0s cone at Mach numbers from 0.5 to 2.0” Metadata:
- Title: ➤ In-flight transition measurement on a 10p0s cone at Mach numbers from 0.5 to 2.0
- Author: David F Fisher
- Language: English
- Number of Pages: Median: 140
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
- Publish Date: 1982
- Publish Location: ➤ Washington, D.C - [Springfield, Va
“In-flight transition measurement on a 10p0s cone at Mach numbers from 0.5 to 2.0” Subjects and Themes:
- Subjects: Boundary layer - Mach number
Edition Identifiers:
- The Open Library ID: OL14933093M - OL17979566M
Access and General Info:
- First Year Published: 1982
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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30Wing pressure distributions from subsonic tests of a high-wing transport model
By Zachary T. Applin
“Wing pressure distributions from subsonic tests of a high-wing transport model” Metadata:
- Title: ➤ Wing pressure distributions from subsonic tests of a high-wing transport model
- Author: Zachary T. Applin
- 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
“Wing pressure distributions from subsonic tests of a high-wing transport model” Subjects and Themes:
- Subjects: ➤ Angle of attack - Leading edge flaps - Mach number - Pressure distribution - Reynolds number - Sideslip - Subsonic flow - Trailing edge flaps - Transport aircraft - Wind tunnel tests - Wings
Edition Identifiers:
- The Open Library ID: OL17788775M - OL15411003M
- Online Computer Library Center (OCLC) ID: 32865600
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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31Invariance of hypersonic normal force coefficients with Reynolds number and determination of inviscid wave drag from laminar experimental results
By Jim A. Penland
“Invariance of hypersonic normal force coefficients with Reynolds number and determination of inviscid wave drag from laminar experimental results” Metadata:
- Title: ➤ Invariance of hypersonic normal force coefficients with Reynolds number and determination of inviscid wave drag from laminar experimental results
- Author: Jim A. Penland
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: Hampton, Va - Springfield, VA
“Invariance of hypersonic normal force coefficients with Reynolds number and determination of inviscid wave drag from laminar experimental results” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Turbulent boundary layer - Aerodynamic coefficients - Body-wing configurations - Reynolds number - Hypersonic forces - Hypersonic boundary layer - Aerodynamic drag - Hypersonic shock - Mach number
Edition Identifiers:
- The Open Library ID: OL17591848M - OL15548849M
- Online Computer Library Center (OCLC) ID: 42677545
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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32Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63
By Jimmy L. Pittman
“Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63” Metadata:
- Title: ➤ Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63
- Author: Jimmy L. Pittman
- Language: English
- Number of Pages: Median: 113
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
- Publish Date: 1980
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63” Subjects and Themes:
- Subjects: Aerodynamics, Supersonic - Hypersonic planes - Mach number - Supersonic Aerodynamics - Supersonic wind tunnels
Edition Identifiers:
- The Open Library ID: OL17651908M - OL17823250M
Access and General Info:
- First Year Published: 1980
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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33An inviscid computational study of three '07 Mars lander aeroshell configurations over a Mach number range of 2.3 to 4.5
By Ramadas K. Prabhu
“An inviscid computational study of three '07 Mars lander aeroshell configurations over a Mach number range of 2.3 to 4.5” Metadata:
- Title: ➤ An inviscid computational study of three '07 Mars lander aeroshell configurations over a Mach number range of 2.3 to 4.5
- Author: Ramadas K. Prabhu
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - Available from NASA Center for AeroSpace Information
- Publish Date: 2001
- Publish Location: Hampton, Va - Hanover, MD
“An inviscid computational study of three '07 Mars lander aeroshell configurations over a Mach number range of 2.3 to 4.5” Subjects and Themes:
- Subjects: ➤ Aeroshells - Computational fluid dynamics - Mars missions - Aerodynamics - Wind tunnel tests - Inviscid flow - Aerodynamic characteristics - Mach number
Edition Identifiers:
- The Open Library ID: OL17719832M - OL17621409M
- Online Computer Library Center (OCLC) ID: 54502386
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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34Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing
By Sheryll Goecke Powers
“Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing” Metadata:
- Title: ➤ Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing
- Author: Sheryll Goecke Powers
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program - National Technical Information Service, distributor]
- Publish Date: 1997
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing” Subjects and Themes:
- Subjects: ➤ Boundary layers - Flight tests - Pressure distribution - Pressure measurement - Swept wings - Angle of attack - Reynolds number - Mach number - Supercritical wings
Edition Identifiers:
- The Open Library ID: OL17839404M - OL15548584M
- Online Computer Library Center (OCLC) ID: 41964681
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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35Supersonic symposium
By Supersonic Symposium (1987 Edwards Air Force Base, Calif.)
“Supersonic symposium” Metadata:
- Title: Supersonic symposium
- Author: ➤ Supersonic Symposium (1987 Edwards Air Force Base, Calif.)
- Languages: ➤ English - Spanish; Castilian - español, castellano
- Number of Pages: Median: 229
- Publisher: ➤ Air Force Flight Test Center History Office
- Publish Date: 1990
- Publish Location: ➤ [Edwards Air Force Base, Calif.]
“Supersonic symposium” Subjects and Themes:
- Subjects: ➤ Aerodynamics, Supersonic - Bell X-1 (Supersonic planes) - Congresses - History - Mach number - Supersonic Aerodynamics - Bell X-1 (Supersonic plane)
- People: Chuck Yeager (1923-)
Edition Identifiers:
- The Open Library ID: OL1666227M - OL14444210M
- Online Computer Library Center (OCLC) ID: 28443674
- Library of Congress Control Number (LCCN): 91600748
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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36Multigrid strategies for viscous flow solvers on anisotropic unstructured meshes
By Dimitri Mavriplis
“Multigrid strategies for viscous flow solvers on anisotropic unstructured meshes” Metadata:
- Title: ➤ Multigrid strategies for viscous flow solvers on anisotropic unstructured meshes
- Author: Dimitri Mavriplis
- Language: English
- Publisher: ➤ Institute for Computer Applications in Science and Engineering, NASA Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: Springfield, VA - Hampton, VA
“Multigrid strategies for viscous flow solvers on anisotropic unstructured meshes” Subjects and Themes:
- Subjects: ➤ Viscous flow - Computational fluid dynamics - Grid generation (Mathematics) - Computational grids - High Reynolds number - Unstructured grids (Mathematics) - Mach number
Edition Identifiers:
- The Open Library ID: OL15547295M - OL17839156M
- Online Computer Library Center (OCLC) ID: 41617780
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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37On the coupling between a supersonic boundary layer and a flexible surface
By Abdelkader Frendi
“On the coupling between a supersonic boundary layer and a flexible surface” Metadata:
- Title: ➤ On the coupling between a supersonic boundary layer and a flexible surface
- Author: Abdelkader Frendi
- Language: English
- Publisher: ➤ Institute for Computer Applications in Science and Engineering, NASA Langley Research Center - National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1992 - 1996
- Publish Location: Hampton, Va - [Springfield, Va
“On the coupling between a supersonic boundary layer and a flexible surface” Subjects and Themes:
- Subjects: ➤ Equilibrium of flexible surfaces - Turbulent boundary layer - Aircraft structures - Flexible bodies - Mathematical models - Computer programs - Supersonic boundary layers - Boundary layer - Mach number - Absorbers (Materials)
Edition Identifiers:
- The Open Library ID: OL14686485M - OL15487233M
Access and General Info:
- First Year Published: 1992
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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38Porous and microporous honeycomb composites as potential boundary-layer bleed materials
By D. O. Davis
“Porous and microporous honeycomb composites as potential boundary-layer bleed materials” Metadata:
- Title: ➤ Porous and microporous honeycomb composites as potential boundary-layer bleed materials
- Author: D. O. Davis
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, D.C
“Porous and microporous honeycomb composites as potential boundary-layer bleed materials” Subjects and Themes:
- Subjects: ➤ Boundary layer control - Honeycomb structures - Composite materials - Supersonic flow - Wind tunnel tests - Mach number
Edition Identifiers:
- The Open Library ID: OL15539875M - OL17838310M
- Online Computer Library Center (OCLC) ID: 40758884
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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39Experimental and theoretical study of flow fields around ducted-nacelle models
By Robert J. Mack
“Experimental and theoretical study of flow fields around ducted-nacelle models” Metadata:
- Title: ➤ Experimental and theoretical study of flow fields around ducted-nacelle models
- Author: Robert J. Mack
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: Hampton, Va - [Springfield, Va
“Experimental and theoretical study of flow fields around ducted-nacelle models” Subjects and Themes:
- Subjects: ➤ Flow characteristics - Angle of attack - Ducted flow - Ducted bodies - Aircraft design - Fluid flow - Mach number - Nacelles
Edition Identifiers:
- The Open Library ID: OL17838725M - OL17700655M
- Online Computer Library Center (OCLC) ID: 41161421
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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40Evaluation 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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41Flow 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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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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42Transonic 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.
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43Robust airfoil optimization to achieve consistent drag reduction over a mach range
By Wu Li
“Robust airfoil optimization to achieve consistent drag reduction over a mach range” Metadata:
- Title: ➤ Robust airfoil optimization to achieve consistent drag reduction over a mach range
- Author: Wu Li
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - Available from NASA Center for AeroSpace Information
- Publish Date: 2001
- Publish Location: Hanover, MD - Hampton, Va
“Robust airfoil optimization to achieve consistent drag reduction over a mach range” Subjects and Themes:
- Subjects: ➤ Aerodynamic drag - Airfoils - Drag reduction - Mach number - Optimization - Robustness (Mathematics)
Edition Identifiers:
- The Open Library ID: OL16050922M - OL17633134M
- Online Computer Library Center (OCLC) ID: 54494222
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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44Investigation of mixing a supersonic stream with the flow downstream of a wedge
By Joseph Sheeley
“Investigation of mixing a supersonic stream with the flow downstream of a wedge” Metadata:
- Title: ➤ Investigation of mixing a supersonic stream with the flow downstream of a wedge
- Author: Joseph Sheeley
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Investigation of mixing a supersonic stream with the flow downstream of a wedge” Subjects and Themes:
- Subjects: ➤ Velocity distribution - Supersonic flow - Flow distribution - Air flow - Flow visualization - Mach number - Gas injection - Multiphase flow - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL15538185M - OL17837879M
- Online Computer Library Center (OCLC) ID: 40563313
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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Downloads Are Not Available:
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45Performance of the 0.3-meter transonic cryogenic tunnel with air, nitrogen, and sulfer hexafluoride media under closed loop automatic control
By Balakrishna, S.
“Performance of the 0.3-meter transonic cryogenic tunnel with air, nitrogen, and sulfer hexafluoride media under closed loop automatic control” Metadata:
- Title: ➤ Performance of the 0.3-meter transonic cryogenic tunnel with air, nitrogen, and sulfer hexafluoride media under closed loop automatic control
- Author: Balakrishna, S.
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1995
- Publish Location: [Springfield, Va - Hampton, Va
“Performance of the 0.3-meter transonic cryogenic tunnel with air, nitrogen, and sulfer hexafluoride media under closed loop automatic control” Subjects and Themes:
- Subjects: ➤ Automatic control - Feedback control - Liquid nitrogen - Mach number - Performance tests - Sulfur hexafluoride - Transonic wind tunnels - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL15409818M - OL18079241M
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:
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46Revised tables of airspeed, altitude, and Mach number presented in the international system of units
By Margaret S. Benner
“Revised tables of airspeed, altitude, and Mach number presented in the international system of units” Metadata:
- Title: ➤ Revised tables of airspeed, altitude, and Mach number presented in the international system of units
- Author: Margaret S. Benner
- Language: English
- Number of Pages: Median: 40
- Publisher: ➤ Scientific and Technical Information Office, National Aeronautics and Space Administration
- Publish Date: 1973
- Publish Location: Washington
“Revised tables of airspeed, altitude, and Mach number presented in the international system of units” Subjects and Themes:
- Subjects: Air speed - Mach number - Tables
Edition Identifiers:
- The Open Library ID: OL5522311M
- Online Computer Library Center (OCLC) ID: 914691
- Library of Congress Control Number (LCCN): 73600284
Access and General Info:
- First Year Published: 1973
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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47Effectiveness of a wedge probe to measure sonic boom signatures in a supersonic wind tunnel
By Floyd J. Wilcox
“Effectiveness of a wedge probe to measure sonic boom signatures in a supersonic wind tunnel” Metadata:
- Title: ➤ Effectiveness of a wedge probe to measure sonic boom signatures in a supersonic wind tunnel
- Author: Floyd J. Wilcox
- Language: English
- Number of Pages: Median: 45
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 2013
- Publish Location: Hampton, Virginia
“Effectiveness of a wedge probe to measure sonic boom signatures in a supersonic wind tunnel” Subjects and Themes:
- Subjects: ➤ Angle of attack - Mach number - Pressure measurement - Sonic booms - Wind tunnel - Wedges
Edition Identifiers:
- The Open Library ID: OL43222313M
- Online Computer Library Center (OCLC) ID: 880925913
Access and General Info:
- First Year Published: 2013
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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48Experimental measurements of sonic boom signatures using a continuous data acquistion technique
By Floyd J. Wilcox
“Experimental measurements of sonic boom signatures using a continuous data acquistion technique” Metadata:
- Title: ➤ Experimental measurements of sonic boom signatures using a continuous data acquistion technique
- Author: Floyd J. Wilcox
- Language: English
- Number of Pages: Median: 45
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 2013
- Publish Location: Hampton, Virginia
“Experimental measurements of sonic boom signatures using a continuous data acquistion technique” Subjects and Themes:
- Subjects: ➤ Angle of attack - Data acquisition - Information flow - Mach number - Reynolds number - Sonic booms - Wind tunnels
Edition Identifiers:
- The Open Library ID: OL43222315M
- Online Computer Library Center (OCLC) ID: 880928070
Access and General Info:
- First Year Published: 2013
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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49Turbulent skin friction at high Mach numbers and Reynolds numbers in air and helium
By Fred W. Matting
“Turbulent skin friction at high Mach numbers and Reynolds numbers in air and helium” Metadata:
- Title: ➤ Turbulent skin friction at high Mach numbers and Reynolds numbers in air and helium
- Author: Fred W. Matting
- Language: English
- Number of Pages: Median: 39
- Publisher: Ames Research Center
- Publish Date: 1961
- Publish Location: Moffett Field, Calif
“Turbulent skin friction at high Mach numbers and Reynolds numbers in air and helium” Subjects and Themes:
- Subjects: Skin friction (Aerodynamics) - Mach number - Reynolds number
Edition Identifiers:
- The Open Library ID: OL57381035M
- Online Computer Library Center (OCLC) ID: 59129894
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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50The stability of radiatively cooling jets
By James M. Stone
“The stability of radiatively cooling jets” Metadata:
- Title: ➤ The stability of radiatively cooling jets
- Author: James M. Stone
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, DC
“The stability of radiatively cooling jets” Subjects and Themes:
- Subjects: ➤ Accretion disks - Cooling flows (Astrophysics) - Hydrodynamics - Kelvin-Helmholtz instability - Mach number - Two dimensional models
Edition Identifiers:
- The Open Library ID: OL15543914M
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:
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