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Source: The Open Library
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1Numerical simulation of the flow about the F-18 HARV at high angle of attack
By Scott M. Murman
“Numerical simulation of the flow about the F-18 HARV at high angle of attack” Metadata:
- Title: ➤ Numerical simulation of the flow about the F-18 HARV at high angle of attack
- Author: Scott M. Murman
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - MCAT Institute - National Aeronautics and Space Administration
- Publish Date: 1994 - 1995
- Publish Location: ➤ [Washington, D.C - Springfield, Va - [Washington, DC - San Jose, CA
“Numerical simulation of the flow about the F-18 HARV at high angle of attack” Subjects and Themes:
- Subjects: ➤ Angle of attack - Computational fluid dynamics - Computational grids - Computerized simulation - F-18 aircraft - Flow geometry - Grid generation (Mathematics) - High Reynolds number - Inlet flow - Leading edge flaps - Mathematical models - Navier-Stokes equation - Numerical analysis - Research aircraft - Research vehicles - Vortex shedding - Vortices
Edition Identifiers:
- The Open Library ID: ➤ OL17683979M - OL17788522M - OL18062579M - OL18081181M - OL17679545M - OL17791646M - OL17683434M - OL17792265M
- Online Computer Library Center (OCLC) ID: 32650521 - 33870418 - 34765697
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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2Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack
By Kenneth W. Iliff
“Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack” Metadata:
- Title: ➤ Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack
- Author: Kenneth W. Iliff
- Language: English
- Number of Pages: Median: 35
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program Center - National Technical Information Service, distributor]
- Publish Date: 1997
- Publish Location: ➤ [Washington, D.C] - [Springfield, Va - [Washington, D.C.]
“Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack” Subjects and Themes:
- Subjects: ➤ Aircraft control - Airplanes - Angle of attack - Angle of attack (Aerodynamics) - Control systems - Directional stability - F-18 aircraft - Hornet (Jet fighter plane) - Lateral Stability of airplanes - Lateral stability - Maximum likelihood estimates - Parameter identification - Research vehicles - Yawing (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL19433480M - OL17127180M - OL18121315M - OL17593988M - OL15504656M
- Online Computer Library Center (OCLC) ID: 40458346
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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3X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data
By Kenneth W. Iliff
“X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data” Metadata:
- Title: ➤ X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data
- Author: Kenneth W. Iliff
- Language: English
- Number of Pages: Median: 35
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program Center - National Aeronautics and Space Administration - National Technical Information Service, distributor]
- Publish Date: 1996
- Publish Location: ➤ [Washington, D.C] - Washington, D.C - [Springfield, Va - [Washington, D.C.]
“X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data” Subjects and Themes:
- Subjects: ➤ Airplanes - Algorithms - Angle of attack - Angle of attack (Aerodynamics) - Control systems - Directional control - Directional stability - Grumman X-29A (Jet plane) - Lateral Stability of airplanes - Lateral control - Lateral stability - Parameter identification - Research aircraft - X-29 aircraft - Yawing (Aerodynamics)
Edition Identifiers:
- The Open Library ID: ➤ OL17135551M - OL17593511M - OL15504500M - OL18121272M - OL20705785M - OL18531287M
- Online Computer Library Center (OCLC) ID: 42787654
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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4Assessment of dual-point drag reduction for an executive-jet modified airfoil section
By Dennis O. Allison
“Assessment of dual-point drag reduction for an executive-jet modified airfoil section” Metadata:
- Title: ➤ Assessment of dual-point drag reduction for an executive-jet modified airfoil section
- Author: Dennis O. Allison
- Language: English
- Number of Pages: Median: 114
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - Available from National Technical Information Center - National Technical Information Service, distributor - National Aeronautics and Space Administration, Langly Research Center
- Publish Date: 1996
- Publish Location: ➤ Hampton, Virginia - Springfield, VA - Hampton, Va - [Springfield, Va
“Assessment of dual-point drag reduction for an executive-jet modified airfoil section” Subjects and Themes:
- Subjects: ➤ Drag reduction - Reynolds number - Boundary layer transition - Angle of attack - Pitching moments - Transonic wind tunnels - Airfoil profiles - Force distribution - Trailing edges - Aerodynamic characteristics - Aerodynamics - Aerofoils
Edition Identifiers:
- The Open Library ID: OL19049550M - OL18121248M - OL17126940M - OL17581020M - OL15504416M
- Online Computer Library Center (OCLC) ID: 40386607
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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5Subsonic analysis of 0.04-scale F-16XL models using an unstructured Euler code
By Wendy B. Lessard
“Subsonic analysis of 0.04-scale F-16XL models using an unstructured Euler code” Metadata:
- Title: ➤ Subsonic analysis of 0.04-scale F-16XL models using an unstructured Euler code
- Author: Wendy B. Lessard
- Language: English
- Number of Pages: Median: 77
- Publisher: ➤ Available from the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ Hampton, Va - Springfield, VA - [Springfield, Va
“Subsonic analysis of 0.04-scale F-16XL models using an unstructured Euler code” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Aircraft models - Pressure distribution - Subsonic flow - Unstructured grids (Mathematics) - Angle of attack - Grid generation (Mathematics) - Flow distribution - Aerodynamics - F-16 (Jet fighter plane) - Wind tunnel models - Mathematics - Numerical grid generation (Numerical analysis)
Edition Identifiers:
- The Open Library ID: OL18121254M - OL17581026M - OL19045641M - OL15504440M - OL17126971M
- Online Computer Library Center (OCLC) ID: 40389824
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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6Evaluation 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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7Low-speed aerodynamic characteristics of a 1/8-scale X-29A airplane model at high angles of attack and side slip
By Raymond D. Whipple
“Low-speed aerodynamic characteristics of a 1/8-scale X-29A airplane model at high angles of attack and side slip” Metadata:
- Title: ➤ Low-speed aerodynamic characteristics of a 1/8-scale X-29A airplane model at high angles of attack and side slip
- Author: Raymond D. Whipple
- Language: English
- Number of Pages: Median: 286
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - Langley Research Center - For sale by the National Technical Information Service]
- Publish Date: 1986
- Publish Location: ➤ Hampton, Va - [Springfield, Va - [Washington, DC]
“Low-speed aerodynamic characteristics of a 1/8-scale X-29A airplane model at high angles of attack and side slip” Subjects and Themes:
- Subjects: Reynolds number - Grumman X-29A (Jet plane) - Forebodies - Swept wings - Angle of attack
Edition Identifiers:
- The Open Library ID: OL17095022M - OL14662026M - OL18028050M - OL20984630M - OL15272847M
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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82-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
Online Access
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9Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring
By Kenneth W. Iliff
“Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring” Metadata:
- Title: ➤ Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring
- Author: Kenneth W. Iliff
- Language: English
- Number of Pages: Median: 65
- Publisher: ➤ National Technical Information Service, distributor - NASA, Dryden Flight Research Center - National Aeronautics and Space Administration, Dryden Flight Research Center - Available from National Technical Information Service
- Publish Date: 1997
- Publish Location: ➤ Edwards, Calif - Springfield, Va - [Springfield, Va
“Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring” Subjects and Themes:
- Subjects: ➤ Aircraft control - Airplanes - Angle of attack - Angle of attack (Aerodynamics) - Control surfaces - Control systems - Flight tests - Hornet (Jet fighter plane) - Longitudinal Stability of airplanes - Longitudinal stability - Maximum likelihood estimates - Parameter identification - Research vehicles - Thrust vector control - Unsteady aerodynamics - Yawing (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL19396278M - OL18134930M - OL17135417M - OL15548785M - OL17591853M
- Online Computer Library Center (OCLC) ID: 42758582
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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10Euler/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
Online Access
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11Evaluation of high-angle-of-attack handling qualities for the X-31A using standard evaluation maneuvers
By Patrick C. Stolike
“Evaluation of high-angle-of-attack handling qualities for the X-31A using standard evaluation maneuvers” Metadata:
- Title: ➤ Evaluation of high-angle-of-attack handling qualities for the X-31A using standard evaluation maneuvers
- Author: Patrick C. Stolike
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Dryden Flight Research Center
- Publish Date: 1996
- Publish Location: ➤ Edwards, Calif - [Springfield, Va
“Evaluation of high-angle-of-attack handling qualities for the X-31A using standard evaluation maneuvers” Subjects and Themes:
- Subjects: ➤ Aircraft maneuvers - Flight control - X-31 aircraft - Aircraft control - Pilot induced oscillation - Flight tests - Angle of attack
Edition Identifiers:
- The Open Library ID: OL15503993M - OL17838754M - OL17128368M - OL18121148M
- Online Computer Library Center (OCLC) ID: 40711821
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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12Two-dimensional high-lift aerodynamic optimization using neural networks
By Roxana M. Greenman
“Two-dimensional high-lift aerodynamic optimization using neural networks” Metadata:
- Title: ➤ Two-dimensional high-lift aerodynamic optimization using neural networks
- Author: Roxana M. Greenman
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: ➤ Springfield, Va - Moffett Field, Calif
“Two-dimensional high-lift aerodynamic optimization using neural networks” Subjects and Themes:
- Subjects: ➤ Aerodynamic coefficients - Computers - Navier-Stokes equation - Lift - Neural nets - Airfoils - Aerodynamic configurations - Angle of attack - Incompressible flow
Edition Identifiers:
- The Open Library ID: OL17129961M - OL17580142M - OL18132744M - OL15542052M
- Online Computer Library Center (OCLC) ID: 41151565
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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13Low-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
Online Access
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14Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel
By Glen P. Doggett
“Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel” Metadata:
- Title: ➤ Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel
- Author: Glen P. Doggett
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: [Springfield, Va - Hampton, Va
“Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel” Subjects and Themes:
- Subjects: ➤ Boundary layer stability - Hypersonics - Aerodynamic stability - Navier-Stokes equation - Hypersonic boundary layer - Hypersonic speed - Aerodynamic noise - Zero angle of attack - Angle of attack
Edition Identifiers:
- The Open Library ID: OL18114813M - OL15487085M - OL17123234M - OL17564495M
- Online Computer Library Center (OCLC) ID: 38994217
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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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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17Navier-Stokes computations on full wing-body configuration with oscillating control surfaces
By Shigeru Obayashi
“Navier-Stokes computations on full wing-body configuration with oscillating control surfaces” Metadata:
- Title: ➤ Navier-Stokes computations on full wing-body configuration with oscillating control surfaces
- Author: Shigeru Obayashi
- Language: English
- Publisher: ➤ [National Aeronautics and Space Administration - National Technical Information Service, distributor - American Institute of Aeronautics and Astronautics
- Publish Date: 1995
- Publish Location: ➤ Washington, DC - Springfield, Va
“Navier-Stokes computations on full wing-body configuration with oscillating control surfaces” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Control surfaces - Transonic flow - Navier-Stokes equation - Arrow wings - Reynolds averaging - Angle of attack
Edition Identifiers:
- The Open Library ID: OL17128605M - OL17578602M - OL15539950M - OL18132117M
- Online Computer Library Center (OCLC) ID: 40771877
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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18Flow-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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19Flight testing the X-36--the test pilot's perspective
By Laurence A. Walker
“Flight testing the X-36--the test pilot's perspective” Metadata:
- Title: ➤ Flight testing the X-36--the test pilot's perspective
- Author: Laurence A. Walker
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor]
- Publish Date: 1997
- Publish Location: ➤ Edwards, Calif - [Springfield, Va
“Flight testing the X-36--the test pilot's perspective” Subjects and Themes:
- Subjects: ➤ Aircraft performance - Angle of attack - Controllability - Flight tests - Fly by wire control - Remotely piloted Vehicles - Thrust vector control
Edition Identifiers:
- The Open Library ID: OL17132642M - OL15548333M - OL18134794M - OL17583321M
- Online Computer Library Center (OCLC) ID: 41936959
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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20F-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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21Low-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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22Low-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
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23Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model
By Stacey J. Cotton
“Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model” Metadata:
- Title: ➤ Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model
- Author: Stacey J. Cotton
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [Springfield, Va - Edwards, Calif
“Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Angle of attack - Buffeting - Flight tests - Flow visualization - Liquid-vapor interfaces - Scale models - Sideslip - Stabilizers (Fluid dynamics) - Tail assemblies - Vortices - Water tunnel tests - X-29 aircraft
Edition Identifiers:
- The Open Library ID: OL17001977M - OL17682958M - OL18076527M
- Online Computer Library Center (OCLC) ID: 32298726
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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24A users guide for the NASA ANOPP Propeller Analysis System
under contract NAS1-96014
By L. Cathy Nguyen
“A users guide for the NASA ANOPP Propeller Analysis System” Metadata:
- Title: ➤ A users guide for the NASA ANOPP Propeller Analysis System
- Author: L. Cathy Nguyen
- Language: English
- Number of Pages: Median: 96
- Publisher: ➤ NASA Langley Research Center - National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Springfield, Va - Hampton, VA - Hampton, Va
“A users guide for the NASA ANOPP Propeller Analysis System” Subjects and Themes:
- Subjects: ➤ Propeller noise - Applications programs (Computers) - Angle of attack - Noise prediction (Aircraft) - Noise - Testing - Airplanes - Computer programs - Aerial Propellers
Edition Identifiers:
- The Open Library ID: OL19394393M - OL17838009M - OL15504971M
- Online Computer Library Center (OCLC) ID: 40238696
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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25A review of hypersonic boundary layer stability experiments in a quiet Mach 6 wind tunnel
By Stephen P. Wilkinson
“A review of hypersonic boundary layer stability experiments in a quiet Mach 6 wind tunnel” Metadata:
- Title: ➤ A review of hypersonic boundary layer stability experiments in a quiet Mach 6 wind tunnel
- Author: Stephen P. Wilkinson
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor - American Institute of Astronautics and Aeronautics
- Publish Date: 1997
- Publish Location: ➤ Reston, VA - [Washington, D.C - Springfield, Va
“A review of hypersonic boundary layer stability experiments in a quiet Mach 6 wind tunnel” Subjects and Themes:
- Subjects: ➤ Pressure gradients - Cooling - Boundary layer stability - Hypersonic boundary layer - Additives - Angle of attack
Edition Identifiers:
- The Open Library ID: OL15503895M - OL18121122M - OL17838510M
- Online Computer Library Center (OCLC) ID: 40426210
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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26Flight-determined, subsonic, lateral-directional stability and control derivatives of the thrust-vectoring F-18 high angle of attack research vehicle (HARV), and comparisons to the basic F-18 and predicted derivates
By Kenneth W. Lliff
“Flight-determined, subsonic, lateral-directional stability and control derivatives of the thrust-vectoring F-18 high angle of attack research vehicle (HARV), and comparisons to the basic F-18 and predicted derivates” Metadata:
- Title: ➤ Flight-determined, subsonic, lateral-directional stability and control derivatives of the thrust-vectoring F-18 high angle of attack research vehicle (HARV), and comparisons to the basic F-18 and predicted derivates
- Author: Kenneth W. Lliff
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor
- Publish Date: 1999
- Publish Location: ➤ Edwards, Calif - Springfield, VA
“Flight-determined, subsonic, lateral-directional stability and control derivatives of the thrust-vectoring F-18 high angle of attack research vehicle (HARV), and comparisons to the basic F-18 and predicted derivates” Subjects and Themes:
- Subjects: ➤ Maximum likelihood estimates - F-18 aircraft - Aircraft control - Directional stability - Control surfaces - Angle of attack
Edition Identifiers:
- The Open Library ID: OL15542746M - OL18132944M - OL17580539M
- Online Computer Library Center (OCLC) ID: 41462984
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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27Application of variable-gain output feedback for high-alpha control
By Aaron J. Ostroff
“Application of variable-gain output feedback for high-alpha control” Metadata:
- Title: ➤ Application of variable-gain output feedback for high-alpha control
- Author: Aaron J. Ostroff
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1990
- Publish Location: Hampton, Va
“Application of variable-gain output feedback for high-alpha control” Subjects and Themes:
- Subjects: ➤ Fighter planes - Control theory - Control systems design - Performance prediction - Flight control - Feedback control - Angle of attack
Edition Identifiers:
- The Open Library ID: OL17726205M - OL17630463M - OL18263186M
- Online Computer Library Center (OCLC) ID: 25037550
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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28Longitudinal-control design approach for high-angle-of-attack aircraft
By Aaron J. Ostroff
“Longitudinal-control design approach for high-angle-of-attack aircraft” Metadata:
- Title: ➤ Longitudinal-control design approach for high-angle-of-attack aircraft
- Author: Aaron J. Ostroff
- Language: English
- Number of Pages: Median: 25
- Publisher: ➤ Langley Research Center - For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1993
- Publish Location: ➤ Hampton, Va - [Springfield, Va - [Washington, DC]
“Longitudinal-control design approach for high-angle-of-attack aircraft” Subjects and Themes:
- Subjects: ➤ Airplanes - Angle of attack - Control systems - Feedback control - Longitudinal Stability of airplanes - Longitudinal control - Stability of airplanes, Longitudinal
Edition Identifiers:
- The Open Library ID: OL19248266M - OL15370896M - OL18057542M
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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29Low-speed stability and control wind-tunnel investigation of effects of spanwise blowing on fighter flight characteristics at high angles of attack
By Dale R. Satran
“Low-speed stability and control wind-tunnel investigation of effects of spanwise blowing on fighter flight characteristics at high angles of attack” Metadata:
- Title: ➤ Low-speed stability and control wind-tunnel investigation of effects of spanwise blowing on fighter flight characteristics at high angles of attack
- Author: Dale R. Satran
- 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.]
“Low-speed stability and control wind-tunnel investigation of effects of spanwise blowing on fighter flight characteristics at high angles of attack” Subjects and Themes:
- Subjects: ➤ Flight characteristics - Spanwise blowing - Low speed stability - Wind tunnel tests - Fighter aircraft - Angle of attack
Edition Identifiers:
- The Open Library ID: OL18468535M - OL16114994M - OL18217699M
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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30Low-speed longitudinal aerodynamic characteristics through poststall for twenty-one novel planform shapes
By Gregory M. Catlin
“Low-speed longitudinal aerodynamic characteristics through poststall for twenty-one novel planform shapes” Metadata:
- Title: ➤ Low-speed longitudinal aerodynamic characteristics through poststall for twenty-one novel planform shapes
- Author: Gregory M. Catlin
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: [Springfield, Va - Hampton, Va
“Low-speed longitudinal aerodynamic characteristics through poststall for twenty-one novel planform shapes” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Angle of attack - Flow visualization - Forebodies - Highly maneuverable aircraft - Lift - Low aspect ratio wings - Low speed - Pitching moments - Swept wings - Wind tunnel tests - Wing planforms
Edition Identifiers:
- The Open Library ID: OL17041056M - OL15426200M - OL18088687M
- Online Computer Library Center (OCLC) ID: 35587781
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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31Installed F/A-18 inlet flow calculations at 30 degrees angle-of-attack, a comparative study
By C. Frederic Smith
“Installed F/A-18 inlet flow calculations at 30 degrees angle-of-attack, a comparative study” Metadata:
- Title: ➤ Installed F/A-18 inlet flow calculations at 30 degrees angle-of-attack, a comparative study
- Author: C. Frederic Smith
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - Lewis Research Center
- Publish Date: 1994
- Publish Location: ➤ [Cleveland, Ohio] - Springfield, Va - [Washington, DC
“Installed F/A-18 inlet flow calculations at 30 degrees angle-of-attack, a comparative study” Subjects and Themes:
- Subjects: ➤ Angle of attack - F-18 aircraft - Highly maneuverable aircraft - Inlet airframe configurations - Inlet flow - Research vehicles - Subsonic speed - Vortices
Edition Identifiers:
- The Open Library ID: OL17000516M - OL18075553M - OL15401957M
- Online Computer Library Center (OCLC) ID: 32062761
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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32Low-speed wind-tunnel investigation of the effect of strakes and nose chines on lateral-directional stability of a fighter configuration
By Jay M. Brandon
“Low-speed wind-tunnel investigation of the effect of strakes and nose chines on lateral-directional stability of a fighter configuration” Metadata:
- Title: ➤ Low-speed wind-tunnel investigation of the effect of strakes and nose chines on lateral-directional stability of a fighter configuration
- Author: Jay M. Brandon
- Language: English
- Number of Pages: Median: 30
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch - Langley Research Center
- Publish Date: 1986
- Publish Location: ➤ Hampton, Va - [Springfield, Va - Washington, D.C
“Low-speed wind-tunnel investigation of the effect of strakes and nose chines on lateral-directional stability of a fighter configuration” Subjects and Themes:
- Subjects: ➤ Angle of attack - Design and construction - Fighter aircraft - Fighter planes - Lateral Stability of airplanes - Lateral stability - Longitudinal stability - Low speed stability - Noses (forebodies) - Stability of airplanes, Lateral - Static tests - Strakes - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL19985921M - OL16152809M - OL18290616M
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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33F-18 high research vehicle (HARV) parameter identification flight test maneuvers for optimal input design validation and lateral control effectiveness
By Eugene A. Morelli
“F-18 high research vehicle (HARV) parameter identification flight test maneuvers for optimal input design validation and lateral control effectiveness” Metadata:
- Title: ➤ F-18 high research vehicle (HARV) parameter identification flight test maneuvers for optimal input design validation and lateral control effectiveness
- Author: Eugene A. Morelli
- 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
“F-18 high research vehicle (HARV) parameter identification flight test maneuvers for optimal input design validation and lateral control effectiveness” Subjects and Themes:
- Subjects: ➤ Aerodynamics - Aircraft control - Aircraft maneuvers - Angle of attack - Dynamic control - F-18 aircraft - Flight tests - Lateral control - Research - Research aircraft
Edition Identifiers:
- The Open Library ID: OL18086961M - OL15423398M
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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34Computation of asymmetric supersonic flows around cones at large incidence
By David Degani
“Computation of asymmetric supersonic flows around cones at large incidence” Metadata:
- Title: ➤ Computation of asymmetric supersonic flows around cones at large incidence
- Author: David Degani
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor - Technion Research & Development Foundation
- Publish Date: 1987
- Publish Location: ➤ Springfield, Va - Technion City, Haifa, Israel - [Washington, D.C
“Computation of asymmetric supersonic flows around cones at large incidence” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Flow equations - Vortices - Supersonic flow - Conical bodies - Navier-Stokes equation - Spatial marching - Conical flow - Angle of attack
Edition Identifiers:
- The Open Library ID: OL17683849M - OL14980900M
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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35A study to determine methods of improving the subsonic performance of a proposed Personnel Launch System (PLS) concept
By Bernard Spencer
“A study to determine methods of improving the subsonic performance of a proposed Personnel Launch System (PLS) concept” Metadata:
- Title: ➤ A study to determine methods of improving the subsonic performance of a proposed Personnel Launch System (PLS) concept
- Author: Bernard Spencer
- 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
“A study to determine methods of improving the subsonic performance of a proposed Personnel Launch System (PLS) concept” Subjects and Themes:
- Subjects: ➤ Launch vehicles - Lift drag ratio - Wind tunnel tests - Subsonic flow - Assured crew return vehicle - Angle of attack - Pitching moments - Lift - Aerodynamic drag - Aerodynamic configurations
Edition Identifiers:
- The Open Library ID: OL17106590M - OL17685249M
- Online Computer Library Center (OCLC) ID: 35281561
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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36Delta wing vortex manipulation using pulsed and steady blowing during ramp pitching
By J. Moreira
“Delta wing vortex manipulation using pulsed and steady blowing during ramp pitching” Metadata:
- Title: ➤ Delta wing vortex manipulation using pulsed and steady blowing during ramp pitching
- Author: J. Moreira
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - Mechanical Engineering Dept., Worcester Polytechnic Institute - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Washington, DC - Springfield, Va - Worcester, MA
“Delta wing vortex manipulation using pulsed and steady blowing during ramp pitching” Subjects and Themes:
- Subjects: Angle of attack - Delta wings - Spanwise blowing - Vortex breakdown - Water tunnel tests
Edition Identifiers:
- The Open Library ID: OL15419012M - OL17793986M
- Online Computer Library Center (OCLC) ID: 34612627
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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37Mechanical design of high lift systems for high aspect ratio swept wings
By Peter K. C. Rudolph
“Mechanical design of high lift systems for high aspect ratio swept wings” Metadata:
- Title: ➤ Mechanical design of high lift systems for high aspect ratio swept wings
- Author: Peter K. C. Rudolph
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“Mechanical design of high lift systems for high aspect ratio swept wings” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Angle of attack - Boeing 757 aircraft - Design analysis - European Airbus - Lift
Edition Identifiers:
- The Open Library ID: OL15548655M - OL17595589M
- Online Computer Library Center (OCLC) ID: 41969370
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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38Flight test of an adaptive configuration optimization system for transport aircraft
By Glenn B. Gilyard
“Flight test of an adaptive configuration optimization system for transport aircraft” Metadata:
- Title: ➤ Flight test of an adaptive configuration optimization system for transport aircraft
- Author: Glenn B. Gilyard
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor
- Publish Date: 1999
- Publish Location: ➤ [Springfield, Va - Edwards, Calif
“Flight test of an adaptive configuration optimization system for transport aircraft” Subjects and Themes:
- Subjects: ➤ Adaptive control - Aerodynamic drag - Aircraft performance - Angle of attack - Cambered wings - Data acquisition - Flight tests - Transport aircraft
Edition Identifiers:
- The Open Library ID: OL17593117M - OL15542421M
- Online Computer Library Center (OCLC) ID: 42042457
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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39Wing 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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40Computational analysis of forebody tangential slot blowing on the high alpha research vehicle
By Ken Gee
“Computational analysis of forebody tangential slot blowing on the high alpha research vehicle” Metadata:
- Title: ➤ Computational analysis of forebody tangential slot blowing on the high alpha research vehicle
- Author: Ken Gee
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - MCAT Institute - National Technical Information Service, distributor
- Publish Date: 1994 - 1995
- Publish Location: ➤ [Washington, DC - San Jose, CA - Springfield, Va
“Computational analysis of forebody tangential slot blowing on the high alpha research vehicle” Subjects and Themes:
- Subjects: ➤ Blowing - Forebodies - Slots - Eddy viscosity - Computational grids - Aerodynamic loads - Research vehicles - Navier-Stokes equation - Transonic flight - F-18 aircraft - Reynolds equation - Directional control - Angle of attack - Yawing moments
Edition Identifiers:
- The Open Library ID: OL18076388M - OL18081178M
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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41Flight 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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42Flutter clearance of the F-18 high-angle-of-attack research vehicle with experimental wingtip instrumentation pods
By Lawrence C. Freudinger
“Flutter clearance of the F-18 high-angle-of-attack research vehicle with experimental wingtip instrumentation pods” Metadata:
- Title: ➤ Flutter clearance of the F-18 high-angle-of-attack research vehicle with experimental wingtip instrumentation pods
- Author: Lawrence C. Freudinger
- Language: English
- Number of Pages: Median: 18
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division
- Publish Date: 1989
- Publish Location: ➤ [Washington, D.C.] - [Springfield, VA
“Flutter clearance of the F-18 high-angle-of-attack research vehicle with experimental wingtip instrumentation pods” Subjects and Themes:
- Subjects: ➤ Vibration - Flutter (Aerodynamics) - Hornet (Jet fighter plane) - Research aircraft - F-18 aircraft - Wing tips - Angle of attack - Clearances - Flutter
Edition Identifiers:
- The Open Library ID: OL17630290M - OL16139104M
- Online Computer Library Center (OCLC) ID: 24899921
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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43High-angle-of-attack yawing movement asymmetry of the X-31 aircraft from flight test
By Brent R. Cobleigh
“High-angle-of-attack yawing movement asymmetry of the X-31 aircraft from flight test” Metadata:
- Title: ➤ High-angle-of-attack yawing movement asymmetry of the X-31 aircraft from flight test
- Author: Brent R. Cobleigh
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor]
- Publish Date: 1994
- Publish Location: ➤ Edwards, Calif - [Springfield, Va
“High-angle-of-attack yawing movement asymmetry of the X-31 aircraft from flight test” Subjects and Themes:
- Subjects: ➤ Aircraft maneuvers - X-31 aircraft - Forebodies - Asymmetry - Dynamic stability - Flight characteristics - Yawing moments - Angle of attack - Flight tests
Edition Identifiers:
- The Open Library ID: OL17001632M - OL18076381M
- Online Computer Library Center (OCLC) ID: 32257091
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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44Effect of actuated forebody strakes on the forebody aerodynamics of the NASA F-18 HARV
By David F. Fisher
“Effect of actuated forebody strakes on the forebody aerodynamics of the NASA F-18 HARV” Metadata:
- Title: ➤ Effect of actuated forebody strakes on the forebody aerodynamics of the NASA F-18 HARV
- Author: David F. Fisher
- Language: English
- Publisher: ➤ National Technical Information Service, distributor] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1996
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Effect of actuated forebody strakes on the forebody aerodynamics of the NASA F-18 HARV” Subjects and Themes:
- Subjects: ➤ F-18 aircraft - Strakes - Pressure distribution - Aerodynamics - Angle of attack - Flow visualization - Leading edges - Yawing moments
Edition Identifiers:
- The Open Library ID: OL15548262M - OL17839408M
- Online Computer Library Center (OCLC) ID: 41975207
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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45Aeroelastic, CFD, and dynamic computation and optimization for buffet and flutter application
By Osama A. Kandil
“Aeroelastic, CFD, and dynamic computation and optimization for buffet and flutter application” Metadata:
- Title: ➤ Aeroelastic, CFD, and dynamic computation and optimization for buffet and flutter application
- Author: Osama A. Kandil
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor - Dept. of Aerospace Engineering, College of Engineering and Technology, Old Dominion University
- Publish Date: 1997
- Publish Location: ➤ [Washington, DC - Norfolk, Va - Springfield, Va
“Aeroelastic, CFD, and dynamic computation and optimization for buffet and flutter application” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Aeroelasticity - Aerospace engineering - Aircraft - Angle of attack - Vortex breakdown
Edition Identifiers:
- The Open Library ID: OL17597464M - OL15547926M
- Online Computer Library Center (OCLC) ID: 42334297
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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46Experimental 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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47Study of the unsteady flow features on a stalled wing
By S. Yon
“Study of the unsteady flow features on a stalled wing” Metadata:
- Title: ➤ Study of the unsteady flow features on a stalled wing
- Author: S. Yon
- Language: English
- Publisher: ➤ American Institute of Aeronautics and Astronautics - National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - Reston, VA - [Washington, DC
“Study of the unsteady flow features on a stalled wing” Subjects and Themes:
- Subjects: ➤ Aerodynamic stalling - Angle of attack - Flow distribution - Frequencies - Rectangular wings - Separated flow - Subsonic wind tunnels - Unsteady flow
Edition Identifiers:
- The Open Library ID: OL15539182M - OL17838077M
- Online Computer Library Center (OCLC) ID: 40832683
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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48A method for integrating thrust-vectoring and actuated forebody strakes with conventional aerodynamic controls on a high-performance fighter airplane
By Frederick J. Lallman
“A method for integrating thrust-vectoring and actuated forebody strakes with conventional aerodynamic controls on a high-performance fighter airplane” Metadata:
- Title: ➤ A method for integrating thrust-vectoring and actuated forebody strakes with conventional aerodynamic controls on a high-performance fighter airplane
- Author: Frederick J. Lallman
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: Springfield, VA - Hampton, Va
“A method for integrating thrust-vectoring and actuated forebody strakes with conventional aerodynamic controls on a high-performance fighter airplane” Subjects and Themes:
- Subjects: ➤ Control stability - Thrust vector control - Feedback control - Angle of attack - Flight control - F-18 aircraft - Directional control - Fighter aircraft - Angular acceleration - Airplanes - Motors - Thrust - Control surfaces
Edition Identifiers:
- The Open Library ID: OL17598638M - OL15542778M
- Online Computer Library Center (OCLC) ID: 42814679
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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49Effectiveness 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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50Experimental 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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