Explore: Wind Tunnel Tests
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Books Results
Source: The Open Library
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Search results from The Open Library
1Hot-jet simulation in cryogenic wind tunnels
By Keisuke Asai
“Hot-jet simulation in cryogenic wind tunnels” Metadata:
- Title: ➤ Hot-jet simulation in cryogenic wind tunnels
- Author: Keisuke Asai
- Language: English
- Number of Pages: Median: 45
- Publisher: ➤ For sale by the National Technical Information Service] - Langley Research Center - National Aeronautics and SpaceAdministration - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division
- Publish Date: 1989
- Publish Location: ➤ Washington D.C - Hampton, Va - Washington, D.C - [Springfield, Va - [Washington, DC]
“Hot-jet simulation in cryogenic wind tunnels” Subjects and Themes:
- Subjects: ➤ Cryogenic wind tunnels - Exhaust flow simulation - Jet flow - Reynolds number - Wind tunnel tests - Wind tunnels
Edition Identifiers:
- The Open Library ID: ➤ OL17683287M - OL19959189M - OL13931490M - OL15576426M - OL18208937M - OL19379736M - OL18078046M - OL1812959M
- Online Computer Library Center (OCLC) ID: 20034307
- Library of Congress Control Number (LCCN): 89602567
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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2Semi-span model testing in the National Transonic Facility
By Ndaona Chokani
“Semi-span model testing in the National Transonic Facility” Metadata:
- Title: ➤ Semi-span model testing in the National Transonic Facility
- Author: Ndaona Chokani
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1993 - 1994 - 1995
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Semi-span model testing in the National Transonic Facility” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Computational grids - Wind tunnel models - Aerodynamics - Wind tunnel tests - Semispan models - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: ➤ OL14700193M - OL18084780M - OL17026142M - OL15385797M - OL17684791M - OL18064500M - OL17793567M
- Online Computer Library Center (OCLC) ID: 34727760 - 34837729
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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3Two-dimensional converging-diverging rippled nozzles at transonic speeds
By John R. Carlson
“Two-dimensional converging-diverging rippled nozzles at transonic speeds” Metadata:
- Title: ➤ Two-dimensional converging-diverging rippled nozzles at transonic speeds
- Author: John R. Carlson
- Language: English
- Number of Pages: Median: 105
- Publisher: ➤ Langley Research Center - National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1994
- Publish Location: ➤ Hampton - Hampton, Va - [Springfield, Va
“Two-dimensional converging-diverging rippled nozzles at transonic speeds” Subjects and Themes:
- Subjects: ➤ Convergent-divergent nozzles - Discharge coefficient - Drag - Nozzle flow - Nozzle geometry - Nozzles - Ripples - Thrust - Trailing edges - Transonic speed - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: ➤ OL19752932M - OL16487219M - OL15403665M - OL16982124M - OL19753709M - OL18076297M
- Online Computer Library Center (OCLC) ID: 32220800
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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41999 NASA High-Speed Research Program Aerodynamic Performance Workshop
By NASA High-Speed Research Program Aerodynamic Performance Workshop (1999 Anaheim, Calif.)
“1999 NASA High-Speed Research Program Aerodynamic Performance Workshop” Metadata:
- Title: ➤ 1999 NASA High-Speed Research Program Aerodynamic Performance Workshop
- Author: ➤ NASA High-Speed Research Program Aerodynamic Performance Workshop (1999 Anaheim, Calif.)
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1999
- Publish Location: Hampton, Va - [Springfield, Va
“1999 NASA High-Speed Research Program Aerodynamic Performance Workshop” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Aerodynamic configurations - Aerodynamic stability - Aerodynamics - Aerodynamics, Supersonic - Aeronautics, Commercial - Aircraft design - Airplanes - Body-wing configurations - Canard configurations - Civil aviation - Commercial Aeronautics - Computational fluid dynamics - Congresses - Design and construction - Engine airframe integration - High-speed aeronautics - Optimization - Performance prediction - Research - Supersonic Aerodynamics - Supersonic transports - Wind tunnel tests - Wing nacelle configurations
Edition Identifiers:
- The Open Library ID: OL18140721M - OL18296463M - OL22405471M - OL15573231M - OL17594870M
- Online Computer Library Center (OCLC) ID: 44596209
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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5Numerical simulation of the SOFIA flowfield
By Stephen P. Klotz
“Numerical simulation of the SOFIA flowfield” Metadata:
- Title: ➤ Numerical simulation of the SOFIA flowfield
- Author: Stephen P. Klotz
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - MCAT Institute - National Aeronautics and Space Administration
- Publish Date: 1994 - 1995
- Publish Location: ➤ Springfield, Va - [Washington, DC - San Jose, CA
“Numerical simulation of the SOFIA flowfield” Subjects and Themes:
- Subjects: ➤ Active control - Aerodynamic stalling - Airfoils - Boeing 747 aircraft - Boundary layer control - Cavities - Flow distribution - Leading edges - SOFIA (Airborne observatory) - Separated flow - Sound pressure - Tail assemblies - Telescopes - Unsteady flow - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL17788523M - OL17791647M - OL18081185M - OL18078541M - OL17683431M
- Online Computer Library Center (OCLC) ID: 33433883 - 32647393
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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6Low-speed wind-tunnel test of an unpowered high-speed stoppable rotor concept in fixed-wing mode
By Michael B. Lance
“Low-speed wind-tunnel test of an unpowered high-speed stoppable rotor concept in fixed-wing mode” Metadata:
- Title: ➤ Low-speed wind-tunnel test of an unpowered high-speed stoppable rotor concept in fixed-wing mode
- Author: Michael B. Lance
- Language: English
- Number of Pages: Median: 51
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - Langley Research Center
- Publish Date: 1991
- Publish Location: ➤ Hampton, Va - [Washington, D.C.]
“Low-speed wind-tunnel test of an unpowered high-speed stoppable rotor concept in fixed-wing mode” Subjects and Themes:
- Subjects: ➤ Testing - Models - Aerodynamics - Convertiplanes - Rotors (Helicopters) - Wind tunnel tests - Helicopter performance - Rotor aerodynamics - Wind tunnel models - Aircraft design - Helicopters
Edition Identifiers:
- The Open Library ID: OL19146711M - OL16125292M - OL17630307M - OL19165536M - OL18227505M
- Online Computer Library Center (OCLC) ID: 60314981
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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7Langley 14- by 22-foot subsonic tunnel test engineer's data acquisition and reduction manual
By P. Frank Quinto
“Langley 14- by 22-foot subsonic tunnel test engineer's data acquisition and reduction manual” Metadata:
- Title: ➤ Langley 14- by 22-foot subsonic tunnel test engineer's data acquisition and reduction manual
- Author: P. Frank Quinto
- Language: English
- Number of Pages: Median: 61
- Publisher: ➤ National Technical Information Service, distributor - Langley Research Center - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1994
- Publish Location: [Springfield, Va - Hampton, Va
“Langley 14- by 22-foot subsonic tunnel test engineer's data acquisition and reduction manual” Subjects and Themes:
- Subjects: Aerodynamics - Wind tunnel tests - Data acquisition - Data reduction
Edition Identifiers:
- The Open Library ID: OL19752685M - OL16998916M - OL17112819M - OL15398210M - OL18072204M
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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8Navier-Stokes, flight, and wind tunnel flow analysis for the F/A-18 aircraft
By Farhad Ghaffari
“Navier-Stokes, flight, and wind tunnel flow analysis for the F/A-18 aircraft” Metadata:
- Title: ➤ Navier-Stokes, flight, and wind tunnel flow analysis for the F/A-18 aircraft
- Author: Farhad Ghaffari
- Language: English
- Number of Pages: Median: 62
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center - Langley Research Center
- Publish Date: 1994
- Publish Location: [Springfield, Va - Hampton, Va
“Navier-Stokes, flight, and wind tunnel flow analysis for the F/A-18 aircraft” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - F-18 aircraft - Vortex breakdown - Vortices - Flow characteristics - Flight tests - Wind tunnel tests - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: OL17114707M - OL19755175M - OL15409376M - OL18079046M - OL16984215M
- Online Computer Library Center (OCLC) ID: 32770362
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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92-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall
By R. A. Piziali
“2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall” Metadata:
- Title: ➤ 2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall
- Author: R. A. Piziali
- Language: English
- Number of Pages: Median: 559
- Publisher: ➤ National Technical Information Service, distributor - Ames Research Center - National Aeronautics and Space Administration, Ames Research Center : US Army Aviation and Troop Command
- Publish Date: 1994
- Publish Location: ➤ Moffett Field, Calif - Moffett Field, Ca - [Springfield, Va
“2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall” Subjects and Themes:
- Subjects: ➤ Rotary wings - Aerodynamic coefficients - Pressure distribution - Wind tunnel tests - Wind oscillations - Angle of attack - Airfoils - Aerodynamic stalling - Semispan models - Stalling - Oscillating wing aerodynamics
Edition Identifiers:
- The Open Library ID: OL17007551M - OL15409387M - OL18079048M - OL19754822M - OL17114716M
- Online Computer Library Center (OCLC) ID: 32770651
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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10Close-range photogrammetric measurement of static deflections for an aeroelastic supercritical wing
By Thomas A. Byrdsong
“Close-range photogrammetric measurement of static deflections for an aeroelastic supercritical wing” Metadata:
- Title: ➤ Close-range photogrammetric measurement of static deflections for an aeroelastic supercritical wing
- Author: Thomas A. Byrdsong
- Language: English
- Number of Pages: Median: 89
- Publisher: ➤ Langley Research Center - National Technical Information Service, distributor] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division
- Publish Date: 1990
- Publish Location: ➤ [Springfield, Va - [Washington, DC] - Hampton, Va
“Close-range photogrammetric measurement of static deflections for an aeroelastic supercritical wing” Subjects and Themes:
- Subjects: ➤ Reflection - Supercritical wings - Photogrammetry - Aeroelasticity - Deflection - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL17114223M - OL18077261M - OL15405511M - OL21334898M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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11Wind-tunnel investigation of a full-scale canard-configured general aviation airplane
By Long P. Yip
“Wind-tunnel investigation of a full-scale canard-configured general aviation airplane” Metadata:
- Title: ➤ Wind-tunnel investigation of a full-scale canard-configured general aviation airplane
- Author: Long P. Yip
- Language: English
- Publisher: ➤ National; Aeronautics and Space Administration Scientific and Technical Information Branch - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1985
- Publish Location: [s.l.] - [Washington, D.C.]
“Wind-tunnel investigation of a full-scale canard-configured general aviation airplane” Subjects and Themes:
- Subjects: ➤ Control stability - Canard configurations - Control surfaces - Wind tunnel tests - General aviation aircraft - Aerodynamic characteristics
Edition Identifiers:
- The Open Library ID: OL13839737M - OL16116833M - OL18218708M
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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12Low-speed wind-tunnel tests of single- and counter-rotation propellers
By Dana Morris Dunham
“Low-speed wind-tunnel tests of single- and counter-rotation propellers” Metadata:
- Title: ➤ Low-speed wind-tunnel tests of single- and counter-rotation propellers
- Author: Dana Morris Dunham
- Language: English
- Number of Pages: Median: 43
- Publisher: ➤ National Aeronautics and Space Administration Scientific and Technical Information Branch - For sale by the National Technical Information Service] - Langley Research Center - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1986
- Publish Location: ➤ Hampton, Va - [Springfield, Va - [s.l.] - [Washington, D.C.]
“Low-speed wind-tunnel tests of single- and counter-rotation propellers” Subjects and Themes:
- Subjects: ➤ Aerial Propellers - Contrarotating propellers - Propeller blades - Propellers - Testing - Turboprop engines - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL16152800M - OL19986671M - OL13841017M - OL18290611M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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13Spin-tunnel investigation of a 1/28-scale model of the NASA F-18 High Alpha Research Vehicle (HARV) with and without vertical tails
By Charles Michael Fremaux
“Spin-tunnel investigation of a 1/28-scale model of the NASA F-18 High Alpha Research Vehicle (HARV) with and without vertical tails” Metadata:
- Title: ➤ Spin-tunnel investigation of a 1/28-scale model of the NASA F-18 High Alpha Research Vehicle (HARV) with and without vertical tails
- Author: Charles Michael Fremaux
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - For sale by the National Technical Information Service
- Publish Date: 1997
- Publish Location: [Springfield, Va - Hampton, Va
“Spin-tunnel investigation of a 1/28-scale model of the NASA F-18 High Alpha Research Vehicle (HARV) with and without vertical tails” Subjects and Themes:
- Subjects: Reynolds number - Wind tunnel tests - Research vehicles - Tail assemblies - Spin tests
Edition Identifiers:
- The Open Library ID: OL17834292M - OL18114842M - OL17123433M - OL15487251M
- Online Computer Library Center (OCLC) ID: 39098301
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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14Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊
By Scott P. Fears
“Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊” Metadata:
- Title: ➤ Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊
- Author: Scott P. Fears
- Language: English
- Number of Pages: Median: 145
- Publisher: ➤ National Aeronautics and Space Administration - Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ Hampton, Va - [Washington, DC - Springfield, Va
“Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊” Subjects and Themes:
- Subjects: ➤ Trailing edge flaps - Aspect ratio - Flight stability tests - Stabilizers (Fluid dynamics) - Wind tunnel tests - Wing profiles - Aerodynamic stability - Angle of attack - Stability - Flight control - Low speed - Planforms - Arrow wings - Tail assemblies - Leading edge flaps
Edition Identifiers:
- The Open Library ID: OL19003591M - OL15416719M - OL18082907M - OL17032232M
- Online Computer Library Center (OCLC) ID: 34127880
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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15Navier-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: ➤ Available from NASA Center for AeroSpace Information - National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service [distributor
- Publish Date: 1999
- Publish Location: ➤ Hanover, MD - Hampton, Va - Springfield, VA
“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: OL17595527M - OL18296120M - OL15569338M - OL18140130M
- 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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16Control of low-speed turbulent separated flow over a backward-facing ramp
By John C. Lin
“Control of low-speed turbulent separated flow over a backward-facing ramp” Metadata:
- Title: ➤ Control of low-speed turbulent separated flow over a backward-facing ramp
- Author: John C. Lin
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Control of low-speed turbulent separated flow over a backward-facing ramp” Subjects and Themes:
- Subjects: ➤ Turbulent flow - Separated flow - Boundary layer separation - Vortices - Flow characteristics - Vortex generators - Horseshoe vortices - Vortex shedding - Low speed - Angle of attack - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL18075631M - OL15402173M - OL17000678M - OL17113743M
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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17A laser-based ice shape profilometer for use in icing wind tunnels
By Edward A. Hovenac
“A laser-based ice shape profilometer for use in icing wind tunnels” Metadata:
- Title: ➤ A laser-based ice shape profilometer for use in icing wind tunnels
- Author: Edward A. Hovenac
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“A laser-based ice shape profilometer for use in icing wind tunnels” Subjects and Themes:
- Subjects: ➤ Laser applications - Ice formation - Wind tunnel tests - Ice - Shapes - Airfoils - Lasers - Wind tunnel models - Leading edges - Profilometers - Imaging techniques
Edition Identifiers:
- The Open Library ID: OL18081560M - OL17116376M - OL15414406M - OL17022695M
- Online Computer Library Center (OCLC) ID: 33958974
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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18Wind-tunnel investigations of blunt-body drug reduction using forebody surface roughness
By Stephen A. Whitmore
“Wind-tunnel investigations of blunt-body drug reduction using forebody surface roughness” Metadata:
- Title: ➤ Wind-tunnel investigations of blunt-body drug reduction using forebody surface roughness
- Author: Stephen A. Whitmore
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Dryden Flight Research Center
- Publish Date: 2001
- Publish Location: ➤ Springfield, VA - Edwards, Calif
“Wind-tunnel investigations of blunt-body drug reduction using forebody surface roughness” Subjects and Themes:
- Subjects: Base flow - Wind tunnel tests - Aerodynamic drag - Drag reduction
Edition Identifiers:
- The Open Library ID: OL18160767M - OL16012016M - OL17601365M - OL18347098M
- Online Computer Library Center (OCLC) ID: 47969712
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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19A Microsoft project-based planning, tracking, and management tool for the National Transonic Facility's model changeover process
By Daniel M. Vairo
“A Microsoft project-based planning, tracking, and management tool for the National Transonic Facility's model changeover process” Metadata:
- Title: ➤ A Microsoft project-based planning, tracking, and management tool for the National Transonic Facility's model changeover process
- Author: Daniel M. Vairo
- 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
“A Microsoft project-based planning, tracking, and management tool for the National Transonic Facility's model changeover process” Subjects and Themes:
- Subjects: Wind tunnel models - Project planning - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL17583592M - OL18134697M - OL17133833M - OL15547880M
- Online Computer Library Center (OCLC) ID: 42250603
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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20Comparison of X-31 flight and ground-based yawing moment asymmetries at high angles of attack
By Brent R. Cobleigh
“Comparison of X-31 flight and ground-based yawing moment asymmetries at high angles of attack” Metadata:
- Title: ➤ Comparison of X-31 flight and ground-based yawing moment asymmetries at high angles of attack
- Author: Brent R. Cobleigh
- Language: English
- Publisher: ➤ Available from NASA Center for AeroSpace Information (CASI) - National Aeronautics and Space Administration, Dryden Flight Research Center
- Publish Date: 2001
- Publish Location: Edwards, Calif - Hanover, MD
“Comparison of X-31 flight and ground-based yawing moment asymmetries at high angles of attack” Subjects and Themes:
- Subjects: ➤ Asymmetry - Flight envelopes - Forebodies - Water tunnel tests - Wind tunnel tests - Yawing moments
Edition Identifiers:
- The Open Library ID: OL18170318M - OL18767809M - OL17615296M - OL17718695M
- Online Computer Library Center (OCLC) ID: 52130350
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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21F-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
Online Access
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22Hot-bench simulation of the active flexible wing wind-tunnel model
By Carey S. Buttrill
“Hot-bench simulation of the active flexible wing wind-tunnel model” Metadata:
- Title: ➤ Hot-bench simulation of the active flexible wing wind-tunnel model
- Author: Carey S. Buttrill
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1990
- Publish Location: Hampton, Va
“Hot-bench simulation of the active flexible wing wind-tunnel model” Subjects and Themes:
- Subjects: Active control - Flexible wings - Wind tunnel models - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL19147025M - OL17628284M - OL18240491M - OL17725451M
- Online Computer Library Center (OCLC) ID: 61669688
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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23User 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
Online Access
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24Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept
By Donald R. Riley
“Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept” Metadata:
- Title: ➤ Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept
- Author: Donald R. Riley
- Language: English
- Number of Pages: Median: 36
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - Langley Research Center - For sale by the National Technical Information Service]
- Publish Date: 1989
- Publish Location: ➤ Hampton, Va - [Springfield, Va - [Washington, D.C.]
“Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept” Subjects and Themes:
- Subjects: ➤ Control systems - Testing - Airplanes - Short take-off and landing aircraft - Hovering - Vertically rising aircraft - Vertical takeoff aircraft - Reaction jets - Jet flow - Wind tunnel tests - Short takeoff aircraft - Fighter aircraft - Attitude control
Edition Identifiers:
- The Open Library ID: OL18269316M - OL17630289M - OL19380199M - OL16140064M
- Online Computer Library Center (OCLC) ID: 24899982
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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25Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 70 ̊
By Holly M. Ross
“Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 70 ̊” Metadata:
- Title: ➤ Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 70 ̊
- Author: Holly M. Ross
- Language: English
- Number of Pages: Median: 140
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - Available from the National Technical Information Service
- Publish Date: 1995
- Publish Location: ➤ Springfield, VA - Hampton, Va - [Springfield, VA
“Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 70 ̊” Subjects and Themes:
- Subjects: ➤ Low aspect ratio wings - Radar cross sections - Wind tunnel tests - Dynamic characteristics - Angle of attack - Tailless aircraft - Sideslip - Low speed - Arrow wings - Airplanes - Wings - Stability of airplanes
Edition Identifiers:
- The Open Library ID: OL19146780M - OL17725194M - OL18227631M - OL17141247M
- Online Computer Library Center (OCLC) ID: 33115440
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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26Fabry-Perot interferometer measurement of static temperature and velocity for ASTOVL model tests
By Helen E. Kourous
“Fabry-Perot interferometer measurement of static temperature and velocity for ASTOVL model tests” Metadata:
- Title: ➤ Fabry-Perot interferometer measurement of static temperature and velocity for ASTOVL model tests
- Author: Helen E. Kourous
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Fabry-Perot interferometer measurement of static temperature and velocity for ASTOVL model tests” Subjects and Themes:
- Subjects: ➤ Fabry-Perot interferometers - Spectrum analysis - Temperature measurement - V/STOL aircraft - Velocity measurement - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL17023004M - OL18081588M - OL15414481M - OL17116420M
- Online Computer Library Center (OCLC) ID: 33973356
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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27Low-speed wind tunnel tests of two waverider configuration models
By Robert J. Pegg
“Low-speed wind tunnel tests of two waverider configuration models” Metadata:
- Title: ➤ Low-speed wind tunnel tests of two waverider configuration models
- Author: Robert J. Pegg
- Language: English
- Publisher: ➤ [National Aeronautics and Space Administration - American Institute of Aeronautics and Astronautics - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ Washington, D.C - Springfield, Va
“Low-speed wind tunnel tests of two waverider configuration models” Subjects and Themes:
- Subjects: ➤ Flight characteristics - Directional stability - Lift drag ratio - Wind tunnel tests - Aircraft configurations - Subsonic speed - Aerodynamic stability - Angle of attack - Pitching moments - Waveriders - Lateral stability - Aerodynamic characteristics
Edition Identifiers:
- The Open Library ID: OL17565252M - OL18118663M - OL15498353M - OL17124624M
- Online Computer Library Center (OCLC) ID: 39554715
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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28Distributed-roughness effects on stability and transition in swept-wing boundary layers
By Ruben B. Carrillo
“Distributed-roughness effects on stability and transition in swept-wing boundary layers” Metadata:
- Title: ➤ Distributed-roughness effects on stability and transition in swept-wing boundary layers
- Author: Ruben B. Carrillo
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Distributed-roughness effects on stability and transition in swept-wing boundary layers” Subjects and Themes:
- Subjects: ➤ Airfoils - Boundary layer stability - Boundary layer transition - Cross flow - Flow visualization - Surface roughness - Swept wings - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL17128387M - OL17597200M - OL18132177M - OL15540242M
- Online Computer Library Center (OCLC) ID: 40717111
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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29Key topics for high-lift research
By David Fisher
“Key topics for high-lift research” Metadata:
- Title: ➤ Key topics for high-lift research
- Author: David Fisher
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Key topics for high-lift research” Subjects and Themes:
- Subjects: ➤ F-15 aircraft - Aerodynamics - Fins - Flow distribution - Lift - Airfoils - Wind tunnel tests - Flight tests
Edition Identifiers:
- The Open Library ID: OL17565560M - OL15492341M - OL17124491M - OL18116300M
- Online Computer Library Center (OCLC) ID: 39517789
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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30The lift-fan aircraft
By W. H. Deckert
“The lift-fan aircraft” Metadata:
- Title: The lift-fan aircraft
- Author: W. H. Deckert
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“The lift-fan aircraft” Subjects and Themes:
- Subjects: ➤ Aerodynamic configurations - Aircraft design - Flight simulation - Lift fans - Propulsion - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL17017590M - OL15413716M - OL18081172M
- Online Computer Library Center (OCLC) ID: 33394644
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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31Supersonic quiet-tunnel development for laminar-turbulent transition research
By Steven P. Schneider
“Supersonic quiet-tunnel development for laminar-turbulent transition research” Metadata:
- Title: ➤ Supersonic quiet-tunnel development for laminar-turbulent transition research
- Author: Steven P. Schneider
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Supersonic quiet-tunnel development for laminar-turbulent transition research” Subjects and Themes:
- Subjects: ➤ Boundary layer equations - Boundary layer transition - Flow characteristics - Flow measurement - Nozzle walls - Supersonic wind tunnels - Wall flow - Wind tunnel nozzles - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL18082383M - OL15415636M - OL17791329M
- Online Computer Library Center (OCLC) ID: 33200505
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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32Two-dimensional aerodynamic characteristics of the NACA 0012 airfoil in the Langley 8-foot transonic pressure tunnel
By Charles D. Harris
“Two-dimensional aerodynamic characteristics of the NACA 0012 airfoil in the Langley 8-foot transonic pressure tunnel” Metadata:
- Title: ➤ Two-dimensional aerodynamic characteristics of the NACA 0012 airfoil in the Langley 8-foot transonic pressure tunnel
- Author: Charles D. Harris
- Number of Pages: Median: 137
- Publisher: Langley Research Center
- Publish Date: 1981
- Publish Location: Hampton, Va
“Two-dimensional aerodynamic characteristics of the NACA 0012 airfoil in the Langley 8-foot transonic pressure tunnel” Subjects and Themes:
- Subjects: Aerodynamic characteristics - Airfoils - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL19750282M - OL21333674M
Access and General Info:
- First Year Published: 1981
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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33Shock-tunnel combustor testing for hypersonic vehicles
By Mark Loomis
“Shock-tunnel combustor testing for hypersonic vehicles” Metadata:
- Title: ➤ Shock-tunnel combustor testing for hypersonic vehicles
- Author: Mark Loomis
- Language: English
- Publisher: ➤ MCAT Institute - National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ Springfield, Va - San Jose, Calif - [Washington, DC
“Shock-tunnel combustor testing for hypersonic vehicles” Subjects and Themes:
- Subjects: ➤ Wind tunnel tests - Two dimensional flow - Hypersonic flow - Supersonic combustion ramjet engines - Propulsion system performance - Propulsion system configurations - Engine tests - Air breathing engines - Hypersonic speed - Combustion chambers - Hypersonic aircraft - Hypersonic inlets - Inlet nozzles - Mach number
Edition Identifiers:
- The Open Library ID: OL17001315M - OL18076085M - OL15403346M
- Online Computer Library Center (OCLC) ID: 32198098
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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34Control 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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35Wind-tunnel evaluation of a 21-percent-scale powered model of a prototype advanced scout helicopter
By Arthur E. Phelps
“Wind-tunnel evaluation of a 21-percent-scale powered model of a prototype advanced scout helicopter” Metadata:
- Title: ➤ Wind-tunnel evaluation of a 21-percent-scale powered model of a prototype advanced scout helicopter
- Author: Arthur E. Phelps
- 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: ➤ Springfield, Va - [Washington, D.C.]
“Wind-tunnel evaluation of a 21-percent-scale powered model of a prototype advanced scout helicopter” Subjects and Themes:
- Subjects: ➤ Military helicopters - Helicopter performance - Wind tunnel tests - Scale models - Aerodynamic characteristics - Stability - Testing - P-531 helicopter
Edition Identifiers:
- The Open Library ID: OL16115009M - OL18217713M - OL18468562M
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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36Performance study for inlet installations
By D. C. Bingaman
“Performance study for inlet installations” Metadata:
- Title: ➤ Performance study for inlet installations
- Author: D. C. Bingaman
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1992
- Publish Location: [Springfield, Va - Hampton, Va
“Performance study for inlet installations” Subjects and Themes:
- Subjects: ➤ Aircraft performance - Engine airframe integration - Aircraft design - Wind tunnel tests - Bomber aircraft - Design analysis - Engine inlets - Aircraft detection - McDonnell aircraft - Fighter aircraft - Inlet airframe configurations
Edition Identifiers:
- The Open Library ID: OL15413640M - OL17791633M
- Online Computer Library Center (OCLC) ID: 33389420
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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37Nacelle-pylon-wing integration on a transport model with a natural laminar flow nacelle
By Milton Lamb
“Nacelle-pylon-wing integration on a transport model with a natural laminar flow nacelle” Metadata:
- Title: ➤ Nacelle-pylon-wing integration on a transport model with a natural laminar flow nacelle
- Author: Milton Lamb
- 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
“Nacelle-pylon-wing integration on a transport model with a natural laminar flow nacelle” Subjects and Themes:
- Subjects: ➤ Statistics - Testing - Laminar flow - Turbulent flow - Pylons - Wing nacelle configurations - Wind tunnel tests - Airplanes - Transonic planes - Nacelles - Wings - Transport aircraft
Edition Identifiers:
- The Open Library ID: OL18217665M - OL18468463M - OL17724275M
- Online Computer Library Center (OCLC) ID: 776151030
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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38Supersonic axial-force characteristics of a rectangular-box cavity with various length-to-depth ratios in a flat plate
By A. B. Blair
“Supersonic axial-force characteristics of a rectangular-box cavity with various length-to-depth ratios in a flat plate” Metadata:
- Title: ➤ Supersonic axial-force characteristics of a rectangular-box cavity with various length-to-depth ratios in a flat plate
- Author: A. B. Blair
- Language: English
- Number of Pages: Median: 18
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service - Langley Research Center
- Publish Date: 1986
- Publish Location: ➤ Hampton, Va - Washington, D.C - Springfield, Va
“Supersonic axial-force characteristics of a rectangular-box cavity with various length-to-depth ratios in a flat plate” Subjects and Themes:
- Subjects: ➤ Aerodynamics, Supersonic - Cavitation flow - Cavities (Airplanes) - Cavity flow - Flat plates - Flow distribution - Flow visualization - Supersonic Aerodynamics - Supersonics - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL19986377M - OL18290608M - OL17727208M
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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39Ultra-high bypass ratio jet noise
By Low, John, K. C.
“Ultra-high bypass ratio jet noise” Metadata:
- Title: ➤ Ultra-high bypass ratio jet noise
- Author: Low, John, K. C.
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Ultra-high bypass ratio jet noise” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - Exhaust nozzles - Wind tunnel tests - Nozzle geometry - Subsonic speed - Bypass ratio - Noise intensity - Noise prediction (Aircraft) - Noise reduction - Jet aircraft noise
Edition Identifiers:
- The Open Library ID: OL17683438M - OL17005197M - OL18078597M
- Online Computer Library Center (OCLC) ID: 32662654
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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40Flow structure generated by perpendicular blade vortex interaction and implications for helicopter noise predictions
By William J. Devenport
“Flow structure generated by perpendicular blade vortex interaction and implications for helicopter noise predictions” Metadata:
- Title: ➤ Flow structure generated by perpendicular blade vortex interaction and implications for helicopter noise predictions
- Author: William J. Devenport
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1994 - 1995
- Publish Location: ➤ Springfield, Va - [Washington, DC - [Washington, D.C
“Flow structure generated by perpendicular blade vortex interaction and implications for helicopter noise predictions” Subjects and Themes:
- Subjects: ➤ Blade slap noise - Blade-vortex interaction - Helicopters - Noise prediction - Rotary wings - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL15413882M - OL17633128M - OL17791704M
- Online Computer Library Center (OCLC) ID: 33450830 - 32031695
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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41Analysis of a six-component, flow-through, strain-gage, force balance used for hypersonic wind tunnel models with scramjet exhaust flow simulation
By Marc W. Kniskern
“Analysis of a six-component, flow-through, strain-gage, force balance used for hypersonic wind tunnel models with scramjet exhaust flow simulation” Metadata:
- Title: ➤ Analysis of a six-component, flow-through, strain-gage, force balance used for hypersonic wind tunnel models with scramjet exhaust flow simulation
- Author: Marc W. Kniskern
- Language: English
- Publisher: ➤ North Carolina State University, Dept. of Mechanical and Aerospace Engineering
- Publish Date: 1990
- Publish Location: Raleigh, [N.C.]
“Analysis of a six-component, flow-through, strain-gage, force balance used for hypersonic wind tunnel models with scramjet exhaust flow simulation” Subjects and Themes:
- Subjects: ➤ Temperature effects - Exhaust flow simulation - Force distribution - Strain gage balances - Gas injection - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL18263150M - OL17632963M - OL16137883M
- Online Computer Library Center (OCLC) ID: 67142056
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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42Viscous-flow analysis of a subsonic transport aircraft high-lift system and correlation with flight data
By R. C. Potter
“Viscous-flow analysis of a subsonic transport aircraft high-lift system and correlation with flight data” Metadata:
- Title: ➤ Viscous-flow analysis of a subsonic transport aircraft high-lift system and correlation with flight data
- Author: R. C. Potter
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - Dept. of Mechanical and Aeronautical Engineering, University of California
- Publish Date: 1995
- Publish Location: ➤ [Washington, DC - Springfield, Va - Davis, CA
“Viscous-flow analysis of a subsonic transport aircraft high-lift system and correlation with flight data” Subjects and Themes:
- Subjects: ➤ Airfoil profiles - Computational grids - Flight tests - Free flow - Navier-Stokes equation - Performance prediction - Swept wings - Three dimensional flow - Transition flow - Two dimensional flow - Viscous flow - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL15418997M - OL18084407M - OL17076220M
- Online Computer Library Center (OCLC) ID: 34776510
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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43Non-linear boundary-layer receptivity due to distributed surface roughness
By Gregory V. Selby
“Non-linear boundary-layer receptivity due to distributed surface roughness” Metadata:
- Title: ➤ Non-linear boundary-layer receptivity due to distributed surface roughness
- Author: Gregory V. Selby
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - Old Dominion University Research Foundation, Dept. of Mechanical Engineering, College of Engineering & Technology - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Washington, D.C - Norfolk, Va - Springfield, Va
“Non-linear boundary-layer receptivity due to distributed surface roughness” Subjects and Themes:
- Subjects: ➤ Boundary layer flow - Boundary layer stability - Boundary layer transition - Laminar boundary layer - Surface roughness - Surface roughness effects - Tollmien-Schlichting waves - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL18084770M - OL15419714M - OL17793565M
- Online Computer Library Center (OCLC) ID: 34736159
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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44Supersonic laminar flow control research
By Ching F. Lo
“Supersonic laminar flow control research” Metadata:
- Title: ➤ Supersonic laminar flow control research
- Author: Ching F. Lo
- Language: English
- Publisher: ➤ Ames Research Center - National Aeronautics and Space Administration - University of Tennessee, Space Institute - National Technical Information Service, distributor
- Publish Date: 1995 - 1996
- Publish Location: ➤ Tullahoma, TN - [Springfield, Va - Moffett Field, CA - [Washington, DC - Springfield, Va
“Supersonic laminar flow control research” Subjects and Themes:
- Subjects: ➤ Boundary layer stability - Supersonic boundary layers - Boundary layer control - Supersonic flow - Laminar flow - Active control - Computational fluid dynamics - Control systems design - Boundary layer flow - Laminar boundary layer - Boundary layer transition - Wind tunnel nozzles - Stability - Temperature distribution - Wind tunnel tests - Laminar boundary - Wall temperature - Supersonic wind tunnels - Prediction analysis techniques - Nozzle design
Edition Identifiers:
- The Open Library ID: OL15543412M - OL15424662M - OL15506457M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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45Orifice-induced pressure error studies in Langley 7- by 10-foot high-speed tunnel
By Elizabeth B. Plentovich
“Orifice-induced pressure error studies in Langley 7- by 10-foot high-speed tunnel” Metadata:
- Title: ➤ Orifice-induced pressure error studies in Langley 7- by 10-foot high-speed tunnel
- Author: Elizabeth B. Plentovich
- Language: English
- Number of Pages: Median: 21
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Infomraton Branch - For sale by the National Technical Information Service] - NASA
- Publish Date: 1986
- Publish Location: ➤ [Washington, D.C.] - Washington - [Springfield, Va
“Orifice-induced pressure error studies in Langley 7- by 10-foot high-speed tunnel” Subjects and Themes:
- Subjects: ➤ Pressure measurement - Flat plates - Orifices - Static pressure - Errors - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL15416239M - OL19985691M - OL18082644M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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46Full-scale semispan tests of a business-jet wing with a natural laminar flow airfoil
By David E. Hahne
“Full-scale semispan tests of a business-jet wing with a natural laminar flow airfoil” Metadata:
- Title: ➤ Full-scale semispan tests of a business-jet wing with a natural laminar flow airfoil
- Author: David E. Hahne
- Language: English
- Number of Pages: Median: 48
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program - Langley Research Center
- Publish Date: 1991
- Publish Location: ➤ [Washington, D.C.] - Springfield, Va - Hampton, Va
“Full-scale semispan tests of a business-jet wing with a natural laminar flow airfoil” Subjects and Themes:
- Subjects: ➤ Laminar flow airfoils - Testing - Jet aircraft - Wind tunnel tests - Airplanes - Full scale tests - Flapping - Airfoil profiles - Laminar flow - Low speed - Semispan models - Wings - Aerofoils
Edition Identifiers:
- The Open Library ID: OL18257128M - OL21499524M - OL16135229M
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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47A two-dimensional adaptive-wall test section with ventilated walls in the Ames 2- by 2-foot transonic wind tunnel
By Edward T. Schairer
“A two-dimensional adaptive-wall test section with ventilated walls in the Ames 2- by 2-foot transonic wind tunnel” Metadata:
- Title: ➤ A two-dimensional adaptive-wall test section with ventilated walls in the Ames 2- by 2-foot transonic wind tunnel
- Author: Edward T. Schairer
- Language: English
- Number of Pages: Median: 56
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - For sale by the National Technical Information Service
- Publish Date: 1989
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“A two-dimensional adaptive-wall test section with ventilated walls in the Ames 2- by 2-foot transonic wind tunnel” Subjects and Themes:
- Subjects: ➤ Wind tunnel walls - Testing - Transonic flow - Wind tunnel tests - Aerodynamic interference - Transonic wind tunnels - Contours - Wall flow
Edition Identifiers:
- The Open Library ID: OL18263200M - OL16138139M - OL17630331M
- Online Computer Library Center (OCLC) ID: 25294414
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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48Wind-tunnel investigation of a flush airdata system at Mach numbers from 0.7 to 1.4
By Terry J. Larson
“Wind-tunnel investigation of a flush airdata system at Mach numbers from 0.7 to 1.4” Metadata:
- Title: ➤ Wind-tunnel investigation of a flush airdata system at Mach numbers from 0.7 to 1.4
- Author: Terry J. Larson
- Language: English
- Number of Pages: Median: 31
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility
- Publish Date: 1990
- Publish Location: ➤ Edwards, Calif - Springfield, VA
“Wind-tunnel investigation of a flush airdata system at Mach numbers from 0.7 to 1.4” Subjects and Themes:
- Subjects: ➤ Aeronautical instruments - Algorithms - Flushing - Air data systems - Wind tunnel tests - Wind tunnels - Flight tests
Edition Identifiers:
- The Open Library ID: OL16138129M - OL18263198M - OL17630323M
- Online Computer Library Center (OCLC) ID: 25269779
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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49Measurements of unsteady pressure and structural response for an elastic supercritical wing
By Clinton V. Eckstrom
“Measurements of unsteady pressure and structural response for an elastic supercritical wing” Metadata:
- Title: ➤ Measurements of unsteady pressure and structural response for an elastic supercritical wing
- Author: Clinton V. Eckstrom
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - For sale by the National Technical Information Service
- Publish Date: 1994
- Publish Location: ➤ Hampton - Hampton, Va - [Springfield, Va
“Measurements of unsteady pressure and structural response for an elastic supercritical wing” Subjects and Themes:
- Subjects: ➤ Aeroelasticity - Dynamic response - Pressure distribution - Supercritical wings - Transonic speed - Unsteady flow - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL15410960M - OL17790670M - OL22824033M
- Online Computer Library Center (OCLC) ID: 32863973
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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50Wind-tunnel results of advanced high-speed propellers at takeoff, climb, and landing Mach numbers
By George L. Stefko
“Wind-tunnel results of advanced high-speed propellers at takeoff, climb, and landing Mach numbers” Metadata:
- Title: ➤ Wind-tunnel results of advanced high-speed propellers at takeoff, climb, and landing Mach numbers
- Author: George L. Stefko
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1985
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Wind-tunnel results of advanced high-speed propellers at takeoff, climb, and landing Mach numbers” Subjects and Themes:
- Subjects: ➤ Prop-fan technology - Efficiency - Turboprop engines - Supersonic wind tunnels - Variable pitch propellers - Energy conservation - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL18078219M - OL17114500M - OL15407426M
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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