Explore: Hovering
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Source: The Open Library
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1XV-15 structural-acoustic data
By Karen H. Lyle
“XV-15 structural-acoustic data” Metadata:
- Title: XV-15 structural-acoustic data
- Author: Karen H. Lyle
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: Hampton, Va - [Springfield, Va
“XV-15 structural-acoustic data” Subjects and Themes:
- Subjects: ➤ Tilting rotors - Horizontal flight - Flight conditions - Ground effect (Aerodynamics) - XV-15 aircraft - Hovering - Acoustic measurement - Noise intensity - Acoustic properties - Flight tests - Nacelles
Edition Identifiers:
- The Open Library ID: OL18131746M - OL17129388M - OL15538664M - OL17592996M
- Online Computer Library Center (OCLC) ID: 40989515
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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2Navier-Stokes flowfield computation of wing/rotor interaction for a tilt rotor aircraft in hover
By Ian G. Fejtek
“Navier-Stokes flowfield computation of wing/rotor interaction for a tilt rotor aircraft in hover” Metadata:
- Title: ➤ Navier-Stokes flowfield computation of wing/rotor interaction for a tilt rotor aircraft in hover
- Author: Ian G. Fejtek
- Language: English
- Number of Pages: Median: 142
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Ames Research Center - Ames Research Center
- Publish Date: 1993
- Publish Location: ➤ [Springfield, Va - Washington, D. C - Moffett Field, Calif
“Navier-Stokes flowfield computation of wing/rotor interaction for a tilt rotor aircraft in hover” Subjects and Themes:
- Subjects: ➤ Fluid dynamics - Rotors - Dynamics - Airplanes - Wings - Hovering - Tilt rotor aircraft
Edition Identifiers:
- The Open Library ID: OL18060967M - OL15379062M - OL14696456M - OL19916692M
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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3Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept
By Donald R. Riley
“Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept” Metadata:
- Title: ➤ Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept
- Author: Donald R. Riley
- Language: English
- Number of Pages: Median: 36
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - Langley Research Center - For sale by the National Technical Information Service]
- Publish Date: 1989
- Publish Location: ➤ Hampton, Va - [Springfield, Va - [Washington, D.C.]
“Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept” Subjects and Themes:
- Subjects: ➤ Control systems - Testing - Airplanes - Short take-off and landing aircraft - Hovering - Vertically rising aircraft - Vertical takeoff aircraft - Reaction jets - Jet flow - Wind tunnel tests - Short takeoff aircraft - Fighter aircraft - Attitude control
Edition Identifiers:
- The Open Library ID: OL18269316M - OL17630289M - OL19380199M - OL16140064M
- Online Computer Library Center (OCLC) ID: 24899982
Access and General Info:
- First Year Published: 1989
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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4Analysis of small-scale rotor hover performance data
By Cahit Kitaplioglu
“Analysis of small-scale rotor hover performance data” Metadata:
- Title: ➤ Analysis of small-scale rotor hover performance data
- Author: Cahit Kitaplioglu
- Language: English
- Number of Pages: Median: 24
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1990
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“Analysis of small-scale rotor hover performance data” Subjects and Themes:
- Subjects: ➤ Rotors (Helicopters) - Hovering - Rotary wings - Test stands - Rotors - Wind effects - Aerodynamics
Edition Identifiers:
- The Open Library ID: OL16135173M - OL18257097M - OL17630348M
- Online Computer Library Center (OCLC) ID: 25291009
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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5Aeroelastic stability of a full-scale hingeless rotor
By Randall L. Peterson
“Aeroelastic stability of a full-scale hingeless rotor” Metadata:
- Title: ➤ Aeroelastic stability of a full-scale hingeless rotor
- Author: Randall L. Peterson
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ Moffett Field, Calif - [Springfield, Va
“Aeroelastic stability of a full-scale hingeless rotor” Subjects and Themes:
- Subjects: ➤ Rotor lift - Rotary wings - Loads (Forces) - Shafts (Machine elements) - Aerodynamic stability - BO-105 helicopter - Hovering - Rigid rotors - Aeroelasticity
Edition Identifiers:
- The Open Library ID: OL15498159M - OL17834422M
- Online Computer Library Center (OCLC) ID: 39705625
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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6Development of time response criteria for rotorcraft at hover and low speed
By David G. Mitchell
“Development of time response criteria for rotorcraft at hover and low speed” Metadata:
- Title: ➤ Development of time response criteria for rotorcraft at hover and low speed
- Author: David G. Mitchell
- Number of Pages: Median: 213
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1985
- Publish Location: New York N. Y
“Development of time response criteria for rotorcraft at hover and low speed” Subjects and Themes:
- Subjects: Hovering - Rotorcraft - Time response
Edition Identifiers:
- The Open Library ID: OL19046394M
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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7Solution method for a hovering helicopter rotor using the Euler equations
By Thomas W. Roberts
“Solution method for a hovering helicopter rotor using the Euler equations” Metadata:
- Title: ➤ Solution method for a hovering helicopter rotor using the Euler equations
- Author: Thomas W. Roberts
- Number of Pages: Median: 12
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1985
- Publish Location: New York
“Solution method for a hovering helicopter rotor using the Euler equations” Subjects and Themes:
- Subjects: Helicopters - Hovering - Rotary blades
Edition Identifiers:
- The Open Library ID: OL21499366M
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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8Experimental and analytical studies of a model helicopter rotor in hover
By Francis X. Caradonna
“Experimental and analytical studies of a model helicopter rotor in hover” Metadata:
- Title: ➤ Experimental and analytical studies of a model helicopter rotor in hover
- Author: Francis X. Caradonna
- Number of Pages: Median: 58
- Publisher: Ames Research Center
- Publish Date: 1981
- Publish Location: Moffett Field, Calif
“Experimental and analytical studies of a model helicopter rotor in hover” Subjects and Themes:
- Subjects: Hovering - Helicopter rotors
Edition Identifiers:
- The Open Library ID: OL22346699M
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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9Free wake analysis of hover performance using a new influence coefficient method
By Todd R. Quackenbush
“Free wake analysis of hover performance using a new influence coefficient method” Metadata:
- Title: ➤ Free wake analysis of hover performance using a new influence coefficient method
- Author: Todd R. Quackenbush
- Number of Pages: Median: 93
- Publisher: Ames Research Center
- Publish Date: 1990
- Publish Location: Moffett Field, Ca
“Free wake analysis of hover performance using a new influence coefficient method” Subjects and Themes:
- Subjects: Helicopter wakes - Rotors - Hovering
Edition Identifiers:
- The Open Library ID: OL21333219M
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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103-D wake measurements near a hovering rotor for determining profile and induced drag
By Kenneth W. McAlister
“3-D wake measurements near a hovering rotor for determining profile and induced drag” Metadata:
- Title: ➤ 3-D wake measurements near a hovering rotor for determining profile and induced drag
- Author: Kenneth W. McAlister
- Number of Pages: Median: 65
- Publisher: ➤ US Army Aviation and Troop Command, Aeroflightdynamics Directorate
- Publish Date: 1995
- Publish Location: Moffett Field, Calif
“3-D wake measurements near a hovering rotor for determining profile and induced drag” Subjects and Themes:
- Subjects: Helicopter wakes - Drag - Rotary wings - Hovering
Edition Identifiers:
- The Open Library ID: OL19005079M
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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11Description of the U.S. Army small-scale 2-meter rotor test system
By Arthur E. Phelps
“Description of the U.S. Army small-scale 2-meter rotor test system” Metadata:
- Title: ➤ Description of the U.S. Army small-scale 2-meter rotor test system
- Author: Arthur E. Phelps
- Number of Pages: Median: 57
- Publisher: Langley Research Center
- Publish Date: 1987
- Publish Location: Hampton, Va
“Description of the U.S. Army small-scale 2-meter rotor test system” Subjects and Themes:
- Subjects: Hovering - Rotary wing aircraft
Edition Identifiers:
- The Open Library ID: OL18998412M
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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12Effects of planform geometry on hover performance of a 2-meter-diameter model of a four-bladed rotor
By Arthur E. Phelps
“Effects of planform geometry on hover performance of a 2-meter-diameter model of a four-bladed rotor” Metadata:
- Title: ➤ Effects of planform geometry on hover performance of a 2-meter-diameter model of a four-bladed rotor
- Author: Arthur E. Phelps
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1986
- Publish Location: [Washington, DC]
“Effects of planform geometry on hover performance of a 2-meter-diameter model of a four-bladed rotor” Subjects and Themes:
- Subjects: ➤ Aerodynamic configurations - Blades - Hovering - Rotor blades (Turbomachinery) - Rotors (Helicopters) - Structural design criteria - Turbomachines
Edition Identifiers:
- The Open Library ID: OL17727205M
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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13Preliminary investigation of motion requirements for the simulation of helicopter hover tasks
By Russell V. Parrish
“Preliminary investigation of motion requirements for the simulation of helicopter hover tasks” Metadata:
- Title: ➤ Preliminary investigation of motion requirements for the simulation of helicopter hover tasks
- Author: Russell V. Parrish
- Number of Pages: Median: 29
- Publisher: Langley Research Center
- Publish Date: 1980
- Publish Location: Hampton, Va
“Preliminary investigation of motion requirements for the simulation of helicopter hover tasks” Subjects and Themes:
- Subjects: Helicopters - Hovering - Flight simulation
Edition Identifiers:
- The Open Library ID: OL22344680M
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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14Stereopsis cueing effects on hover-in-turbulence performance in a simulated rotorcraft
By Russell V. Parrish
“Stereopsis cueing effects on hover-in-turbulence performance in a simulated rotorcraft” Metadata:
- Title: ➤ Stereopsis cueing effects on hover-in-turbulence performance in a simulated rotorcraft
- Author: Russell V. Parrish
- Language: English
- Number of Pages: Median: 59
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - For sale by the National Technical Information Service
- Publish Date: 1990
- Publish Location: ➤ Washington, D.C - Springfield, Va
“Stereopsis cueing effects on hover-in-turbulence performance in a simulated rotorcraft” Subjects and Themes:
- Subjects: ➤ Helicopters - Cues - Flight simulation - Display systems - Display devices - Hovering - Three-dimensional display systems - Piloting - Stereoscope - Pilot performance - Aerodynamics - Helicopter flight simulators - Rotary wing aircraft - Computer simulation - Aeronautical instruments - Turbulence
Edition Identifiers:
- The Open Library ID: OL16137785M
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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15Performance and pressure data from a small model tilt-rotor in hover
By Lonnie Branum
“Performance and pressure data from a small model tilt-rotor in hover” Metadata:
- Title: ➤ Performance and pressure data from a small model tilt-rotor in hover
- Author: Lonnie Branum
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Springfield, Va - Moffett Field, CA
“Performance and pressure data from a small model tilt-rotor in hover” Subjects and Themes:
- Subjects: Tilting rotors - Pressure measurement - Hovering - Pressure distribution - Tilt rotor aircraft
Edition Identifiers:
- The Open Library ID: OL15500640M
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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16The effects of structural flap-lag and pitch-lag coupling on soft inplane hingeless rotor stability in hover
By William G. Bousman
“The effects of structural flap-lag and pitch-lag coupling on soft inplane hingeless rotor stability in hover” Metadata:
- Title: ➤ The effects of structural flap-lag and pitch-lag coupling on soft inplane hingeless rotor stability in hover
- Author: William G. Bousman
- Language: English
- Number of Pages: Median: 56
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - For sale by the National Technical Information Service]
- Publish Date: 1990
- Publish Location: ➤ Washington, D.C - [Springfield, Va
“The effects of structural flap-lag and pitch-lag coupling on soft inplane hingeless rotor stability in hover” Subjects and Themes:
- Subjects: ➤ Rotors (Helicopters) - Rotary wings - Coupling - Aerodynamics - Stability - Hovering stability - Hovering - Mathematical models - Rigid rotors - Aeroelasticity
Edition Identifiers:
- The Open Library ID: OL16131128M
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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17Wide speed range turboshaft study
By Martin D'Angelo
“Wide speed range turboshaft study” Metadata:
- Title: ➤ Wide speed range turboshaft study
- Author: Martin D'Angelo
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“Wide speed range turboshaft study” Subjects and Themes:
- Subjects: ➤ Tilting rotors - Engine design - Cruising flight - Rotor speed - Gas turbine engines - Propeller efficiency - Hovering - Turboshafts - Tilt rotor aircraft - Transport aircraft
Edition Identifiers:
- The Open Library ID: OL15425905M
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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18Navier-Stokes calculations of the flowfield of a helicopter rotor in hover
By R. K. Agarwal
“Navier-Stokes calculations of the flowfield of a helicopter rotor in hover” Metadata:
- Title: ➤ Navier-Stokes calculations of the flowfield of a helicopter rotor in hover
- Author: R. K. Agarwal
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1988
- Publish Location: Washington
“Navier-Stokes calculations of the flowfield of a helicopter rotor in hover” Subjects and Themes:
- Subjects: Helicopters - Hovering - Rotary wings - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: OL19916404M
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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19Navier-Stokes calculations for the vortex wake of a rotor in hover
By Chen Huei Liu
“Navier-Stokes calculations for the vortex wake of a rotor in hover” Metadata:
- Title: ➤ Navier-Stokes calculations for the vortex wake of a rotor in hover
- Author: Chen Huei Liu
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1993
- Publish Location: New York
“Navier-Stokes calculations for the vortex wake of a rotor in hover” Subjects and Themes:
- Subjects: Aircraft wakes - Rotors - Hovering - Navier-Stokes equation - Vortices
Edition Identifiers:
- The Open Library ID: OL19916947M
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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20Design and evaluation of a cockpit display for hovering flight
By Ronald A. Hess
“Design and evaluation of a cockpit display for hovering flight” Metadata:
- Title: ➤ Design and evaluation of a cockpit display for hovering flight
- Author: Ronald A. Hess
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1988
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Design and evaluation of a cockpit display for hovering flight” Subjects and Themes:
- Subjects: ➤ Display devices - Hovering - Flight simulation - Military helicopters - Evaluation - Cockpits - Design analysis
Edition Identifiers:
- The Open Library ID: OL17683183M
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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21Euler solutions to nonlinear acoustics of non-lifting hovering rotor blades
By J. D. Baeder
“Euler solutions to nonlinear acoustics of non-lifting hovering rotor blades” Metadata:
- Title: ➤ Euler solutions to nonlinear acoustics of non-lifting hovering rotor blades
- Author: J. D. Baeder
- Language: English
- Publisher: ➤ US Army Aviation Systems Command, Aviation Research and Technology Activity - National Aeronautics and Space Administration, Ames Research Center - For sale by the National Technical Information Service, distributor
- Publish Date: 1991
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“Euler solutions to nonlinear acoustics of non-lifting hovering rotor blades” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Rotor aerodynamics - Nonlinearity - Blade tips - Rotor blades (Turbomachinery) - Stability - Hovering - Acoustic properties - Euler equations of motion
Edition Identifiers:
- The Open Library ID: OL17114268M
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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22Flow field around a hovering rotor
By C. Tung
“Flow field around a hovering rotor” Metadata:
- Title: ➤ Flow field around a hovering rotor
- Author: C. Tung
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“Flow field around a hovering rotor” Subjects and Themes:
- Subjects: ➤ Velocity distribution - Unsteady flow - Helicopter wakes - Applications programs (Computers) - Flow distribution - Hovering - Prediction analysis techniques - Downwash
Edition Identifiers:
- The Open Library ID: OL15498168M
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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23A two dimensional study of rotor/airfoil interaction in hover
By Chyang Sheng Lee
“A two dimensional study of rotor/airfoil interaction in hover” Metadata:
- Title: ➤ A two dimensional study of rotor/airfoil interaction in hover
- Author: Chyang Sheng Lee
- Language: English
- Publisher: ➤ Stanford University - National Technical Information Service, distributor - National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1988
- Publish Location: ➤ Moffett Field, Calif - [Palo Alto, Calif.] - [Springfield, Va
“A two dimensional study of rotor/airfoil interaction in hover” Subjects and Themes:
- Subjects: ➤ Hovering - Hovercraft ground effect machines - Airfoil profiles - Ground effect (Aerodynamics) - Two dimensional models - Interactional aerodynamics
Edition Identifiers:
- The Open Library ID: OL15409844M
Access and General Info:
- First Year Published: 1988
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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24Rotor vortex filaments
By Larry A. Young
“Rotor vortex filaments” Metadata:
- Title: Rotor vortex filaments
- Author: Larry A. Young
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“Rotor vortex filaments” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Rotary wing aircraft - Axial flow - Vortex filaments - Shear layers - Hovering - Slipstreams
Edition Identifiers:
- The Open Library ID: OL15484312M
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
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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25Documentation of ice shapes on the main rotor of a UH-1H helicopter in hover
By John D. Lee
“Documentation of ice shapes on the main rotor of a UH-1H helicopter in hover” Metadata:
- Title: ➤ Documentation of ice shapes on the main rotor of a UH-1H helicopter in hover
- Author: John D. Lee
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Lewis Research Center
- Publish Date: 1984
- Publish Location: [Cleveland, Ohio]
“Documentation of ice shapes on the main rotor of a UH-1H helicopter in hover” Subjects and Themes:
- Subjects: Hovering - Ice formation - Rotary wings - UH-1 helicopter
Edition Identifiers:
- The Open Library ID: OL16122268M
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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26Moving base simulation evaluation of translational rate command systems for STOVL aircraft in hover
By James A. Franklin
“Moving base simulation evaluation of translational rate command systems for STOVL aircraft in hover” Metadata:
- Title: ➤ Moving base simulation evaluation of translational rate command systems for STOVL aircraft in hover
- Author: James A. Franklin
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“Moving base simulation evaluation of translational rate command systems for STOVL aircraft in hover” Subjects and Themes:
- Subjects: ➤ Command guidance - Flight characteristics - Flight control - Hovering - STOVL aircraft - V/STOL aircraft - Vertical motion simulators
Edition Identifiers:
- The Open Library ID: OL15498145M
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
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27Revised simulation model of the control system, displays, and propulsion system for an ASTOVL lift fan aircraft
By James A. Franklin
“Revised simulation model of the control system, displays, and propulsion system for an ASTOVL lift fan aircraft” Metadata:
- Title: ➤ Revised simulation model of the control system, displays, and propulsion system for an ASTOVL lift fan aircraft
- Author: James A. Franklin
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“Revised simulation model of the control system, displays, and propulsion system for an ASTOVL lift fan aircraft” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Command and control - Control equipment - Control theory - Display devices - Fighter aircraft - Flight characteristics - Flight simulation - Head-up displays - Hovering - Lift fans - Propulsion - Takeoff - Vertical landing
Edition Identifiers:
- The Open Library ID: OL15498463M
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
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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