Explore: Control Surfaces
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Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1Methods for estimating stability and control derivatives of conventional subsonic airplanes
By Jan Roskam
“Methods for estimating stability and control derivatives of conventional subsonic airplanes” Metadata:
- Title: ➤ Methods for estimating stability and control derivatives of conventional subsonic airplanes
- Author: Jan Roskam
- Language: English
- Publisher: ➤ Roskam Aviation and Engineering Corp.]
- Publish Date: 1971 - 1983
- Publish Location: [Lawrence? Kan - [Ottawa, Kan
“Methods for estimating stability and control derivatives of conventional subsonic airplanes” Subjects and Themes:
- Subjects: Airplanes - Control surfaces - Stability of airplanes
Edition Identifiers:
- The Open Library ID: OL4584346M - OL16511295M
- Library of Congress Control Number (LCCN): 77173352
Access and General Info:
- First Year Published: 1971
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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2Optimal pitch thrust-vector angle and benefits for all flight regimes
By Glenn B. Gilyard
“Optimal pitch thrust-vector angle and benefits for all flight regimes” Metadata:
- Title: ➤ Optimal pitch thrust-vector angle and benefits for all flight regimes
- Author: Glenn B. Gilyard
- Language: English
- Number of Pages: Median: 22
- Publisher: ➤ National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor
- Publish Date: 2000
- Publish Location: ➤ [Springfield, Va - Edwards, Calif
“Optimal pitch thrust-vector angle and benefits for all flight regimes” Subjects and Themes:
- Subjects: ➤ Airplanes - Angles (Geometry) - Automatic flight control - Control surfaces - Drag (Aerodynamics) - Flight testing - Handling characteristics - Lift (Aerodynamics) - Motors - Pitch (Inclination) - Thrust - Thrust vector control
Edition Identifiers:
- The Open Library ID: ➤ OL17704162M - OL20639635M - OL17596831M - OL18318816M - OL18302177M - OL18140962M
- Online Computer Library Center (OCLC) ID: 45009655
Access and General Info:
- First Year Published: 2000
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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3Control-surface hinge-moment calculations for a high-aspect-ratio supercritical wing
By Boyd Perry
“Control-surface hinge-moment calculations for a high-aspect-ratio supercritical wing” Metadata:
- Title: ➤ Control-surface hinge-moment calculations for a high-aspect-ratio supercritical wing
- Author: Boyd Perry
- Language: English
- Number of Pages: Median: 23
- Publisher: ➤ for sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Office
- Publish Date: 1978
- Publish Location: Springfield, Va - [Washington]
“Control-surface hinge-moment calculations for a high-aspect-ratio supercritical wing” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL15228380M - OL17977132M - OL14925492M - OL17118914M - OL18014344M
Access and General Info:
- First Year Published: 1978
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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4Flight-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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5Microfabricated ice-detection sensor
By Russell G. DeAnna
“Microfabricated ice-detection sensor” Metadata:
- Title: ➤ Microfabricated ice-detection sensor
- Author: Russell G. DeAnna
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Microfabricated ice-detection sensor” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL18121070M - OL17579553M - OL17129564M - OL15503670M
- Online Computer Library Center (OCLC) ID: 41031153
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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6Wind-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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7Navier-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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8X-38 vehicle 131 flutter assessment
By James P. Smith - undifferentiated
“X-38 vehicle 131 flutter assessment” Metadata:
- Title: ➤ X-38 vehicle 131 flutter assessment
- Author: ➤ James P. Smith - undifferentiated
- Language: English
- Number of Pages: Median: 23
- Publisher: ➤ National Aeronautics and Space Administration, Lyndon B. Johnson Space Center - National Aeronautics and Space Administration - National Technical Information Service, distributor - Lyndon B. Johnson Space Center - Available from the Center for AeroSpace Information]
- Publish Date: 1997
- Publish Location: ➤ Washington, D.C - [Springfield, Va - [Houston, Tex.] - [Linthicum Heights, MD
“X-38 vehicle 131 flutter assessment” Subjects and Themes:
- Subjects: ➤ Aerodynamic balance - Aerodynamic characteristics - Aerodynamic forces - Airplanes - Control surfaces - Damping - Fins - Flutter (Aerodynamics) - Flutter analysis - Launch vehicles (Astronautics) - Mathematical models - Reusable space vehicles - Rudders - X-38 crew return vehicle
Edition Identifiers:
- The Open Library ID: OL18502902M - OL17125520M - OL17569015M - OL19158282M
- Online Computer Library Center (OCLC) ID: 39850867
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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9Laser scanning system for pressure and temperature paints
By John Sullivan
“Laser scanning system for pressure and temperature paints” Metadata:
- Title: ➤ Laser scanning system for pressure and temperature paints
- Author: John Sullivan
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Laser scanning system for pressure and temperature paints” Subjects and Themes:
- Subjects: ➤ Pressure distribution - Paints - Aerospace vehicles - Spatial resolution - High resolution - Pressure measurement - Control surfaces - Aerodynamics
Edition Identifiers:
- The Open Library ID: OL17837386M - OL17697854M - OL17126090M
- Online Computer Library Center (OCLC) ID: 40109522
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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10Flight-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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11Aerothermal environment in chordwise gaps between split elevons at Mach 6.8
By L. Roane Hunt
“Aerothermal environment in chordwise gaps between split elevons at Mach 6.8” Metadata:
- Title: ➤ Aerothermal environment in chordwise gaps between split elevons at Mach 6.8
- Author: L. Roane Hunt
- Language: English
- Number of Pages: Median: 42
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
- Publish Date: 1980
- Publish Location: ➤ [Springfield, Va - Washington, D.C
“Aerothermal environment in chordwise gaps between split elevons at Mach 6.8” Subjects and Themes:
- Subjects: Control surfaces - Aerothermodynamics - Airplanes - Turbulent boundary layer - Reusable space vehicles
Edition Identifiers:
- The Open Library ID: OL17823251M - OL14932815M - OL17651909M
Access and General Info:
- First Year Published: 1980
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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12The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil
By Charles D. Harris
“The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil” Metadata:
- Title: ➤ The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil
- Author: Charles D. Harris
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Division
- Publish Date: 1988
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil” Subjects and Themes:
- Subjects: Control surfaces - Airplanes - Aerofoils
Edition Identifiers:
- The Open Library ID: OL18028660M - OL15274214M - OL16371185M
Access and General Info:
- First Year Published: 1988
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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13Performance of an electro-hydrostatic actuator on the F-18 systems research aircraft
By Robert Navarro
“Performance of an electro-hydrostatic actuator on the F-18 systems research aircraft” Metadata:
- Title: ➤ Performance of an electro-hydrostatic actuator on the F-18 systems research aircraft
- Author: Robert Navarro
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Dryden Flight Research Center
- Publish Date: 1997
- Publish Location: ➤ [Springfield, Va - Edwards, Calif
“Performance of an electro-hydrostatic actuator on the F-18 systems research aircraft” Subjects and Themes:
- Subjects: ➤ Actuators - Control surfaces - Electric motors - F-18 aircraft - Flight control - Flight tests - Ground tests - Hydraulic equipment - Hydrostatics - Research aircraft - Systems engineering
Edition Identifiers:
- The Open Library ID: OL17838520M - OL15503773M
- Online Computer Library Center (OCLC) ID: 41153931
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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14Automated optimum design of wing structures
deterministic and probabilistic approaches
By Rao, S. S.
“Automated optimum design of wing structures” Metadata:
- Title: ➤ Automated optimum design of wing structures
- Author: Rao, S. S.
- 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]
- Publish Date: 1982
- Publish Location: ➤ Washington, D.C - [Springfield, Va
“Automated optimum design of wing structures” Subjects and Themes:
- Subjects: Mathematical models - Airplanes - Control surfaces - Wings - Design and construction
Edition Identifiers:
- The Open Library ID: OL17662472M - OL17800040M
Access and General Info:
- First Year Published: 1982
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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15Proceedings of the Circulation-Control Workshop, 1986
By Circulation-Control Workshop (1986 Ames Research Center)
“Proceedings of the Circulation-Control Workshop, 1986” Metadata:
- Title: ➤ Proceedings of the Circulation-Control Workshop, 1986
- Author: ➤ Circulation-Control Workshop (1986 Ames Research Center)
- Language: English
- Number of Pages: Median: 599
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Branch - For sale by National Technical Information Service
- Publish Date: 1987
- Publish Location: ➤ [Springfield, Va - Springfield, Va - Washington, D.C
“Proceedings of the Circulation-Control Workshop, 1986” Subjects and Themes:
- Subjects: Aerofoils - Airplanes - Congresses - Control surfaces
Edition Identifiers:
- The Open Library ID: OL2494879M - OL17682254M
- Library of Congress Control Number (LCCN): 87601972
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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16Aerodynamics of combat aircraft controls and of ground effects
By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
“Aerodynamics of combat aircraft controls and of ground effects” Metadata:
- Title: ➤ Aerodynamics of combat aircraft controls and of ground effects
- Author: ➤ North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
- Language: English
- Number of Pages: Median: 340
- Publisher: AGARD
- Publish Date: 1990
- Publish Location: ➤ Neuilly-sur-Seine - Neuilly sur Seine, France
“Aerodynamics of combat aircraft controls and of ground effects” Subjects and Themes:
- Subjects: Aerodynamic characteristics - Control surfaces - Fighter aircraft
Edition Identifiers:
- The Open Library ID: OL21333584M - OL20116980M
- All ISBNs: 9789283505556 - 9283505557
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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17Instability and transition of flow at, and near, an attachment-line
By A. Smith
“Instability and transition of flow at, and near, an attachment-line” Metadata:
- Title: ➤ Instability and transition of flow at, and near, an attachment-line
- Author: A. Smith
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996 - 1998
- Publish Location: ➤ Hampton, Va - [Washington, DC - [Springfield, Va - Springfield, Va
“Instability and transition of flow at, and near, an attachment-line” Subjects and Themes:
- Subjects: ➤ Boundary layer control - Boundary layer transition - Boundary layers - Control surfaces - Drag - Laminar boundary layer - Reynolds number - Stability - Transition flow - Turbulence - Wings
Edition Identifiers:
- The Open Library ID: OL15544664M - OL15547327M
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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18Precision controllability of the FY-17 airplane
By Thomas R. Sisk
“Precision controllability of the FY-17 airplane” Metadata:
- Title: ➤ Precision controllability of the FY-17 airplane
- Author: Thomas R. Sisk
- Language: English
- Number of Pages: Median: 31
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Office - For sale by the National Technical Information Service]
- Publish Date: 1980
- Publish Location: ➤ [Springfield, Va - Washington, D.C
“Precision controllability of the FY-17 airplane” Subjects and Themes:
- Subjects: Testing - Airplanes - Handling characteristics - Control systems - Control surfaces
Edition Identifiers:
- The Open Library ID: OL17652943M - OL17544116M
Access and General Info:
- First Year Published: 1980
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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19Thermal control surfaces experiment
By Donald R. Wilkes
“Thermal control surfaces experiment” Metadata:
- Title: ➤ Thermal control surfaces experiment
- Author: Donald R. Wilkes
- Language: English
- Publisher: ➤ National Technical Information Service [distributor - National Aeronautics and Space Administration, Marshall Space Flight Center
- Publish Date: 1999
- Publish Location: ➤ Springfield, VA - [Huntsville], Ala
“Thermal control surfaces experiment” Subjects and Themes:
- Subjects: ➤ Control surfaces - Cooling systems - Environmental engineering - Infrared suppression - Long Duration Exposure Facility - Temperature control
Edition Identifiers:
- The Open Library ID: OL17597488M - OL15548020M
- Online Computer Library Center (OCLC) ID: 42242913
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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20Stability and control characteristics of a three-surface advanced fighter configuration at angles of attack up to 45⁰
By William P. Henderson
“Stability and control characteristics of a three-surface advanced fighter configuration at angles of attack up to 45⁰” Metadata:
- Title: ➤ Stability and control characteristics of a three-surface advanced fighter configuration at angles of attack up to 45⁰
- Author: William P. Henderson
- Language: English
- Number of Pages: Median: 44
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1981
- Publish Location: ➤ Washington, D.C - Springfield, Va
“Stability and control characteristics of a three-surface advanced fighter configuration at angles of attack up to 45⁰” Subjects and Themes:
- Subjects: Control surfaces - Stability of airplanes - Flight testing - Fighter planes - Airplanes
Edition Identifiers:
- The Open Library ID: OL17654709M - OL17799193M
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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21Testing and optimization of electrically conductive spacecraft coatings
By R. J. Mell
“Testing and optimization of electrically conductive spacecraft coatings” Metadata:
- Title: ➤ Testing and optimization of electrically conductive spacecraft coatings
- Author: R. J. Mell
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Marshall Space Flight Center
- Publish Date: 2001
- Publish Location: MSFC, Ala
“Testing and optimization of electrically conductive spacecraft coatings” Subjects and Themes:
- Subjects: ➤ Space vehicles - Electrostatic charging - Protective coatings - Thermal properties - Materials - Electrical resistivity - Thermal control coatings - Temperature control - Control surfaces
Edition Identifiers:
- The Open Library ID: OL17621407M - OL16042480M
- Online Computer Library Center (OCLC) ID: 54502411
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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22Non-linear unsteady wing theory
By J. E. McCune
“Non-linear unsteady wing theory” Metadata:
- Title: ➤ Non-linear unsteady wing theory
- Author: J. E. McCune
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1987
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Non-linear unsteady wing theory” Subjects and Themes:
- Subjects: ➤ Aircraft maneuvers - Computational fluid dynamics - Unsteady flow - Control surfaces - Interactional aerodynamics - Wings - Aerodynamic characteristics
Edition Identifiers:
- The Open Library ID: OL17683867M - OL18080139M
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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23Low-speed wind-tunnel investigation of a porous forebody and nose strakes for yaw control of a multirole fighter aircraft
By Scott P. Fears
“Low-speed wind-tunnel investigation of a porous forebody and nose strakes for yaw control of a multirole fighter aircraft” Metadata:
- Title: ➤ Low-speed wind-tunnel investigation of a porous forebody and nose strakes for yaw control of a multirole fighter aircraft
- Author: Scott P. Fears
- Language: English
- Number of Pages: Median: 88
- Publisher: ➤ Available from the National Technical Information Service - Langley Research Center - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1995
- Publish Location: Hampton, Va - Springfield, VA
“Low-speed wind-tunnel investigation of a porous forebody and nose strakes for yaw control of a multirole fighter aircraft” Subjects and Themes:
- Subjects: Control surfaces - Yaw - Fighter aircraft - Airplanes - Yawing (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL17141129M - OL19003971M
- Online Computer Library Center (OCLC) ID: 33165427
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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24Computational study of the aerodynamics and control by blowing of asymmetric vortical flows over Delta wings
By Ken Craig
“Computational study of the aerodynamics and control by blowing of asymmetric vortical flows over Delta wings” Metadata:
- Title: ➤ Computational study of the aerodynamics and control by blowing of asymmetric vortical flows over Delta wings
- Author: Ken Craig
- Language: English
- Number of Pages: Median: 37
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - Stanford University, Dept. of Aeronautics and Astronautics
- Publish Date: 1991
- Publish Location: ➤ Stanford, Calif - [Moffett Field, Calif.?]
“Computational study of the aerodynamics and control by blowing of asymmetric vortical flows over Delta wings” Subjects and Themes:
- Subjects: ➤ Unsteady flow (Aerodynamics) - Airplanes - Delta wing airplanes - Control surfaces - Equilibrium flow - Upper surface blowing - Turbulence models - Wing profiles - Flow distribution - Delta wings - Grid generation (Mathematics)
Edition Identifiers:
- The Open Library ID: OL16137796M - OL17633070M
- Online Computer Library Center (OCLC) ID: 34364710
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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25A 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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26Steady and unsteady transonic pressure measurements on a clipped delta wing for pitching and control-surface oscillations
By R. W. Hess
“Steady and unsteady transonic pressure measurements on a clipped delta wing for pitching and control-surface oscillations” Metadata:
- Title: ➤ Steady and unsteady transonic pressure measurements on a clipped delta wing for pitching and control-surface oscillations
- Author: R. W. Hess
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service,]
- Publish Date: 1986
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Steady and unsteady transonic pressure measurements on a clipped delta wing for pitching and control-surface oscillations” Subjects and Themes:
- Subjects: ➤ Control surfaces - Delta wings - Longitudinal control - Oscillations - Pressure measurement - Steady state - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL16116604M
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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27Discussion on the paper "Some aspects of propulsion for the augmenter-wing concept (NASA-CR-125540, by D.C. Whittley)"
By H. Schmitt
“Discussion on the paper "Some aspects of propulsion for the augmenter-wing concept (NASA-CR-125540, by D.C. Whittley)"” Metadata:
- Title: ➤ Discussion on the paper "Some aspects of propulsion for the augmenter-wing concept (NASA-CR-125540, by D.C. Whittley)"
- Author: H. Schmitt
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1985
- Publish Location: ➤ Washington D.C - [Springfield, Va
“Discussion on the paper "Some aspects of propulsion for the augmenter-wing concept (NASA-CR-125540, by D.C. Whittley)"” Subjects and Themes:
- Subjects: Airplanes - Control surfaces
Edition Identifiers:
- The Open Library ID: OL15396179M
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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28Characteristics of aft-mounted all-moving rectangular control surfaces on a slender cruciform model at mach numbers from 0.6 to 2.8
By Kenneth George Winter
“Characteristics of aft-mounted all-moving rectangular control surfaces on a slender cruciform model at mach numbers from 0.6 to 2.8” Metadata:
- Title: ➤ Characteristics of aft-mounted all-moving rectangular control surfaces on a slender cruciform model at mach numbers from 0.6 to 2.8
- Author: Kenneth George Winter
- Language: English
- Number of Pages: Median: 108
- Publisher: H.M.S.O.
- Publish Date: 1968
- Publish Location: London
“Characteristics of aft-mounted all-moving rectangular control surfaces on a slender cruciform model at mach numbers from 0.6 to 2.8” Subjects and Themes:
- Subjects: Airplanes - Control surfaces - Cruciform Wings - Supersonic Aerodynamics
Edition Identifiers:
- The Open Library ID: OL5515135M
- Library of Congress Control Number (LCCN): 73463313
Access and General Info:
- First Year Published: 1968
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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29A wind-tunnel investigation of static longitudinal and lateral characteristics of a full-scale mockup of a light twin-engine airplane
By Marvin P. Fink
“A wind-tunnel investigation of static longitudinal and lateral characteristics of a full-scale mockup of a light twin-engine airplane” Metadata:
- Title: ➤ A wind-tunnel investigation of static longitudinal and lateral characteristics of a full-scale mockup of a light twin-engine airplane
- Author: Marvin P. Fink
- Language: English
- Number of Pages: Median: 268
- Publisher: ➤ National Aeronautics and Space Administration; [for sale by the National Technical Information Service, Springfield, Va.]
- Publish Date: 1971
- Publish Location: Washington
“A wind-tunnel investigation of static longitudinal and lateral characteristics of a full-scale mockup of a light twin-engine airplane” Subjects and Themes:
- Subjects: Airplanes - Control surfaces - Stability of airplanes - Wind tunnels
Edition Identifiers:
- The Open Library ID: OL5276210M
- Library of Congress Control Number (LCCN): 71612136
Access and General Info:
- First Year Published: 1971
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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30The control characteristics of aircraft employing direct-lift control
By W. J. G. Pinsker
“The control characteristics of aircraft employing direct-lift control” Metadata:
- Title: ➤ The control characteristics of aircraft employing direct-lift control
- Author: W. J. G. Pinsker
- Language: English
- Number of Pages: Median: 57
- Publisher: H.M. Stationery Off.
- Publish Date: 1970
- Publish Location: London
“The control characteristics of aircraft employing direct-lift control” Subjects and Themes:
- Subjects: Airplanes - Control surfaces - Lift (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL5006518M
- Library of Congress Control Number (LCCN): 76522828
Access and General Info:
- First Year Published: 1970
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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31Analysis of unsteady pressure measurements on a supercritical airfoil with a harmonically oscillating trailing edge flap at subsonic and transonic speeds
By H. Sundara Murthy
“Analysis of unsteady pressure measurements on a supercritical airfoil with a harmonically oscillating trailing edge flap at subsonic and transonic speeds” Metadata:
- Title: ➤ Analysis of unsteady pressure measurements on a supercritical airfoil with a harmonically oscillating trailing edge flap at subsonic and transonic speeds
- Author: H. Sundara Murthy
- Language: English
- Number of Pages: Median: 78
- Publisher: DFVLR
- Publish Date: 1984
- Publish Location: Köln
“Analysis of unsteady pressure measurements on a supercritical airfoil with a harmonically oscillating trailing edge flap at subsonic and transonic speeds” Subjects and Themes:
- Subjects: Aerofoils - Airplanes - Control surfaces - Flaps (Airplanes)
Edition Identifiers:
- The Open Library ID: OL47988975M
- Online Computer Library Center (OCLC) ID: 17660672
Access and General Info:
- First Year Published: 1984
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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32Development of selected advanced aerodynamics and active control concepts for commercial transport airfcraft
By A. B. Taylor
“Development of selected advanced aerodynamics and active control concepts for commercial transport airfcraft” Metadata:
- Title: ➤ Development of selected advanced aerodynamics and active control concepts for commercial transport airfcraft
- Author: A. B. Taylor
- Language: English
- Publisher: ➤ National Technical Information Service, distributor] - National Aeronautics and Space Administration, Scientific and Technical Information Office
- Publish Date: 1984
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Development of selected advanced aerodynamics and active control concepts for commercial transport airfcraft” Subjects and Themes:
- Subjects: Aerodynamics - Airplanes - Control surfaces - Transport planes
Edition Identifiers:
- The Open Library ID: OL15391919M
Access and General Info:
- First Year Published: 1984
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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33Investigation of vortex flaps and other flow control devices on generic high-speed civil transport planforms
By Kevin J. Kjerstad
“Investigation of vortex flaps and other flow control devices on generic high-speed civil transport planforms” Metadata:
- Title: ➤ Investigation of vortex flaps and other flow control devices on generic high-speed civil transport planforms
- Author: Kevin J. Kjerstad
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - Available from NASA Center for AeroSpace Information - National Technical Information Service [distributor
- Publish Date: 1999
- Publish Location: ➤ Springfield, VA - Hanover, MD - Hampton, Va
“Investigation of vortex flaps and other flow control devices on generic high-speed civil transport planforms” Subjects and Themes:
- Subjects: ➤ Vortex flaps - High speed - Planforms - Subsonic wind tunnels - Computational fluid dynamics - Control surfaces - Civil aviation
Edition Identifiers:
- The Open Library ID: OL15569332M
- Online Computer Library Center (OCLC) ID: 44440801
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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34Assessment of lift augmentation devices
By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development
“Assessment of lift augmentation devices” Metadata:
- Title: ➤ Assessment of lift augmentation devices
- Author: ➤ North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development
- Language: English
- Publisher: ➤ North Atlantic Treaty Organization, Advisory Group for Aerospace Research and Development
- Publish Date: 1971
- Publish Location: [Neuilly-sur-Seine, France]
“Assessment of lift augmentation devices” Subjects and Themes:
- Subjects: Lift (Aerodynamics) - Congresses - Airplanes - Aerofoils - Control surfaces
Edition Identifiers:
- The Open Library ID: OL5164513M
- Library of Congress Control Number (LCCN): 74590574
Access and General Info:
- First Year Published: 1971
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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35Aėromekhanicheskiĭ kontrolʹ
By Vladimir Zhivetin
“Aėromekhanicheskiĭ kontrolʹ” Metadata:
- Title: Aėromekhanicheskiĭ kontrolʹ
- Author: Vladimir Zhivetin
- Language: rus
- Number of Pages: Median: 195
- Publisher: [publisher not identified]
- Publish Date: 2000
- Publish Location: Kazanʹ
“Aėromekhanicheskiĭ kontrolʹ” Subjects and Themes:
- Subjects: Airplanes - Performance - Control surfaces - Aerodynamics
Edition Identifiers:
- The Open Library ID: OL30994140M
- Library of Congress Control Number (LCCN): 2013484182
- All ISBNs: 5898200142 - 9785898200145
Access and General Info:
- First Year Published: 2000
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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36Periodische Optimalflugbahn mit singulärer Steuerung
By Klaus Lesch
“Periodische Optimalflugbahn mit singulärer Steuerung” Metadata:
- Title: ➤ Periodische Optimalflugbahn mit singulärer Steuerung
- Author: Klaus Lesch
- Language: ger
- Number of Pages: Median: 162
- Publisher: Utz, Wissenschaft
- Publish Date: 1996
- Publish Location: München
“Periodische Optimalflugbahn mit singulärer Steuerung” Subjects and Themes:
- Subjects: Control surfaces - Mathematical optimization - Airplanes
Edition Identifiers:
- The Open Library ID: OL31450334M
- Library of Congress Control Number (LCCN): 98188585
- All ISBNs: 3896751204 - 9783896751201
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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37Active load control during rolling maneuvers
By Jessica A. Woods-Vedeler
“Active load control during rolling maneuvers” Metadata:
- Title: ➤ Active load control during rolling maneuvers
- Author: Jessica A. Woods-Vedeler
- Language: English
- Publisher: ➤ National Technical Information Service [distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1994
- Publish Location: Springfield, VA - Hampton, Va
“Active load control during rolling maneuvers” Subjects and Themes:
- Subjects: ➤ Aerodynamic loads - Control surfaces - Wind tunnel tests - Flexible wings - Active control - Wing loading - Roll
Edition Identifiers:
- The Open Library ID: OL15408536M
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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38Launch vehicle flight control augmentation using smart materials and advanced composites (CDDF project 93-05)
By Chris Barret
“Launch vehicle flight control augmentation using smart materials and advanced composites (CDDF project 93-05)” Metadata:
- Title: ➤ Launch vehicle flight control augmentation using smart materials and advanced composites (CDDF project 93-05)
- Author: Chris Barret
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1995
- Publish Location: Hampton, Va - [Springfield, Va
“Launch vehicle flight control augmentation using smart materials and advanced composites (CDDF project 93-05)” Subjects and Themes:
- Subjects: ➤ Smart structures - Flight control - Spacecraft construction materials - Launch vehicles - Control surfaces - Spacecraft design - Composite structures
Edition Identifiers:
- The Open Library ID: OL15415982M
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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39Aerodynamic characteristics of airplanes at high angles of attack
By Joseph R Chambers
“Aerodynamic characteristics of airplanes at high angles of attack” Metadata:
- Title: ➤ Aerodynamic characteristics of airplanes at high angles of attack
- Author: Joseph R Chambers
- Language: English
- Number of Pages: Median: 94
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Office - for sale by the National Technical Information Service
- Publish Date: 1977
- Publish Location: [Washington] - Springfield, Va
“Aerodynamic characteristics of airplanes at high angles of attack” Subjects and Themes:
- Subjects: Control surfaces - Stability of airplanes - Airplanes - Spin (Aerodynamics) - Stalling (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL14925206M
Access and General Info:
- First Year Published: 1977
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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40Theoretical study of the effect of wind velocity gradients on longitudinal stability and control in climbing and level flight
By Windsor L Sherman
“Theoretical study of the effect of wind velocity gradients on longitudinal stability and control in climbing and level flight” Metadata:
- Title: ➤ Theoretical study of the effect of wind velocity gradients on longitudinal stability and control in climbing and level flight
- Author: Windsor L Sherman
- Language: English
- Number of Pages: Median: 18
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Office - for sale by the National Technical Information Service
- Publish Date: 1978
- Publish Location: [Washington] - Springfield, Va
“Theoretical study of the effect of wind velocity gradients on longitudinal stability and control in climbing and level flight” Subjects and Themes:
- Subjects: Winds - Control surfaces - Airplanes
Edition Identifiers:
- The Open Library ID: OL14932219M
Access and General Info:
- First Year Published: 1978
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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41Stability and control characteristics of a three-surface advanced fighter configuration at angles of attack up to 45p0s
By William P Henderson
“Stability and control characteristics of a three-surface advanced fighter configuration at angles of attack up to 45p0s” Metadata:
- Title: ➤ Stability and control characteristics of a three-surface advanced fighter configuration at angles of attack up to 45p0s
- Author: William P Henderson
- Language: English
- Number of Pages: Median: 44
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1981
- Publish Location: ➤ Washington, D.C - Springfield, Va
“Stability and control characteristics of a three-surface advanced fighter configuration at angles of attack up to 45p0s” Subjects and Themes:
- Subjects: Control surfaces - Stability of airplanes - Flight testing - Fighter planes - Airplanes
Edition Identifiers:
- The Open Library ID: OL14925810M
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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42Automated optimum design of wing structures
By S. S Rao
“Automated optimum design of wing structures” Metadata:
- Title: ➤ Automated optimum design of wing structures
- Author: S. S Rao
- Language: English
- Number of Pages: Median: 43
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1982
- Publish Location: ➤ Washington, D.C - [Springfield, Va
“Automated optimum design of wing structures” Subjects and Themes:
- Subjects: Mathematical models - Airplanes - Control surfaces - Wings - Design and construction
Edition Identifiers:
- The Open Library ID: OL14926123M
Access and General Info:
- First Year Published: 1982
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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43Forebody tangential blowing for control at high angles of attack
By Ilan Kroo
“Forebody tangential blowing for control at high angles of attack” Metadata:
- Title: ➤ Forebody tangential blowing for control at high angles of attack
- Author: Ilan Kroo
- Language: English
- Number of Pages: Median: 34
- Publisher: ➤ Stanford University, Dept. of Aeronautics and Astronautics - National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1991
- Publish Location: ➤ [Moffett Field, Calif.] - Stanford, CA
“Forebody tangential blowing for control at high angles of attack” Subjects and Themes:
- Subjects: Control surfaces - Flight control - Airplanes - Aerodynamics
Edition Identifiers:
- The Open Library ID: OL15382867M
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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44The aerodynamics of controls
By A. D. Young
“The aerodynamics of controls” Metadata:
- Title: The aerodynamics of controls
- Author: A. D. Young
- Number of Pages: Median: 15
- Publisher: Sine nomine
- Publish Date: 1984
- Publish Location: [S.l.]
“The aerodynamics of controls” Subjects and Themes:
- Subjects: Aerodynamics - Control surfaces
Edition Identifiers:
- The Open Library ID: OL19987814M
Access and General Info:
- First Year Published: 1984
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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45Computer modeling of time-dependent rime icing in the atmosphere
By Edward P. Lozowski
“Computer modeling of time-dependent rime icing in the atmosphere” Metadata:
- Title: ➤ Computer modeling of time-dependent rime icing in the atmosphere
- Author: Edward P. Lozowski
- Language: English
- Number of Pages: Median: 74
- Publisher: ➤ U.S. Army Corps of Engineers, Cold Regions Research & Engineering Laboratory
- Publish Date: 1983
- Publish Location: [Hanover, N.H.]
“Computer modeling of time-dependent rime icing in the atmosphere” Subjects and Themes:
- Subjects: Airplanes - Control surfaces - Icing (Meteorology) - Cold weather operation
Edition Identifiers:
- The Open Library ID: OL17552778M
Access and General Info:
- First Year Published: 1983
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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46Structural tests and development of a laminar flow control wing surface composite chordwise joint
By L. B. Lineberger
“Structural tests and development of a laminar flow control wing surface composite chordwise joint” Metadata:
- Title: ➤ Structural tests and development of a laminar flow control wing surface composite chordwise joint
- Author: L. B. Lineberger
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - Lockheed-Georgia Company
- Publish Date: 1984
- Publish Location: Hampton, Va - Marietta, Ga
“Structural tests and development of a laminar flow control wing surface composite chordwise joint” Subjects and Themes:
- Subjects: ➤ Laminar flow - Laminar boundary layer - Boundary layer control - Control surfaces - Structural analysis - Airplanes - Composite structures
Edition Identifiers:
- The Open Library ID: OL16157026M
Access and General Info:
- First Year Published: 1984
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
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47A computer module used to calculate the horizontal control surface size of a conceputal aircraft design
By Doral R. Sandlin
“A computer module used to calculate the horizontal control surface size of a conceputal aircraft design” Metadata:
- Title: ➤ A computer module used to calculate the horizontal control surface size of a conceputal aircraft design
- Author: Doral R. Sandlin
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - California Polytechnic State University, Aeronautical Engineering Dept. - National Aeronautics and Space Administration
- Publish Date: 1990
- Publish Location: ➤ San Luis Obispo, Calif - [Washington, D.C.] - [Springfield, Va
“A computer module used to calculate the horizontal control surface size of a conceputal aircraft design” Subjects and Themes:
- Subjects: ➤ Mathematical models - Computer aided design - Canard configurations - Aircraft design.. - Control surfaces - Computer programs - Design analysis
Edition Identifiers:
- The Open Library ID: OL16138013M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
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48A concept for adaptive performance optimization on commercial transport aircraft
By Michael R. Jackson
“A concept for adaptive performance optimization on commercial transport aircraft” Metadata:
- Title: ➤ A concept for adaptive performance optimization on commercial transport aircraft
- Author: Michael R. Jackson
- Language: English
- Publisher: ➤ National Technical Information Service, distributor] - National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - Edwards, Calif
“A concept for adaptive performance optimization on commercial transport aircraft” Subjects and Themes:
- Subjects: ➤ Transport aircraft - Drag reduction - Monte Carlo method - Aerodynamic drag - Cambered wings - Commercial aircraft - Control surfaces - Adaptive control - Least squares method
Edition Identifiers:
- The Open Library ID: OL15423362M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
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49Effect of control surface mass unbalance on the stability of a closed-loop active control system
By E. Nissim
“Effect of control surface mass unbalance on the stability of a closed-loop active control system” Metadata:
- Title: ➤ Effect of control surface mass unbalance on the stability of a closed-loop active control system
- Author: E. Nissim
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - National Technical Information Service, distributor]
- Publish Date: 1989
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Effect of control surface mass unbalance on the stability of a closed-loop active control system” Subjects and Themes:
- Subjects: ➤ Aerodynamics - Feedback control - Aerodynamic stability - Flutter - Mass distribution - Control surfaces - Balance - Inertia - Active control
Edition Identifiers:
- The Open Library ID: OL15402406M
Access and General Info:
- First Year Published: 1989
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
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50Linear and angular position measurement of aircraft components
By J. C. P. van der Linden
“Linear and angular position measurement of aircraft components” Metadata:
- Title: ➤ Linear and angular position measurement of aircraft components
- Author: J. C. P. van der Linden
- Language: English
- Number of Pages: Median: 41
- Publisher: AGARD, NATO
- Publish Date: 1977
- Publish Location: Neuilly sur Seine
“Linear and angular position measurement of aircraft components” Subjects and Themes:
- Subjects: Airplanes - Control surfaces - Control systems
Edition Identifiers:
- The Open Library ID: OL19692477M
- All ISBNs: 9283512368
Access and General Info:
- First Year Published: 1977
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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