Explore: Aircraft Models
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Source: The Open Library
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1Subsonic 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
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2Low-order nonlinear dynamic model of IC engine-variable pitch propeller system for general aviation aircraft
By Jacques C. Richard
“Low-order nonlinear dynamic model of IC engine-variable pitch propeller system for general aviation aircraft” Metadata:
- Title: ➤ Low-order nonlinear dynamic model of IC engine-variable pitch propeller system for general aviation aircraft
- Author: Jacques C. Richard
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Low-order nonlinear dynamic model of IC engine-variable pitch propeller system for general aviation aircraft” Subjects and Themes:
- Subjects: ➤ Flight simulation - Aircraft models - Propulsion system performance - Single engine aircraft - Variable pitch propellers - Internal combustion engines - General aviation aircraft - Dynamic models
Edition Identifiers:
- The Open Library ID: OL17087697M - OL15420716M - OL18085503M - OL17116925M
- Online Computer Library Center (OCLC) ID: 34614216
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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3Acoustic treatment design scaling methods
By R. E. Kraft
“Acoustic treatment design scaling methods” Metadata:
- Title: ➤ Acoustic treatment design scaling methods
- Author: R. E. Kraft
- 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 - 2003
- Publish Location: ➤ - Hanover, MD - [Springfield, Va - Hampton, Va
“Acoustic treatment design scaling methods” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - High frequencies - Mathematical models - Aircraft models - Scale models - Aircraft engines - Acoustic impedance - Frequency ranges - Aircraft noise - Noise prediction (Aircraft) - Impedance measurement - Acoustic properties
Edition Identifiers:
- The Open Library ID: OL17621421M - OL17722881M - OL15554930M - OL17584196M
- Online Computer Library Center (OCLC) ID: 54914469 - 42269573
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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4Computer-aided light sheet flow visualization using photogrammetry
By Kathryn Stacy
“Computer-aided light sheet flow visualization using photogrammetry” Metadata:
- Title: ➤ Computer-aided light sheet flow visualization using photogrammetry
- Author: Kathryn Stacy
- Language: English
- Number of Pages: Median: 33
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center - Langley Research Center
- Publish Date: 1994
- Publish Location: Hampton, Va - [Springfield, Va
“Computer-aided light sheet flow visualization using photogrammetry” Subjects and Themes:
- Subjects: ➤ Aircraft models - Cameras - Computer graphics - Computer techniques - Descriptive Geometry - Digital techniques - Flow visualization - Image processing - Image reconstruction - Photogrammetry
Edition Identifiers:
- The Open Library ID: OL15404329M - OL18076531M - OL19752987M - OL16982107M
- Online Computer Library Center (OCLC) ID: 32298795
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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5Structural dynamic model obtained from flight use with piloted simulation and handling qualities analysis
By Bruce G. Powers
“Structural dynamic model obtained from flight use with piloted simulation and handling qualities analysis” Metadata:
- Title: ➤ Structural dynamic model obtained from flight use with piloted simulation and handling qualities analysis
- Author: Bruce G. Powers
- 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.]
“Structural dynamic model obtained from flight use with piloted simulation and handling qualities analysis” Subjects and Themes:
- Subjects: ➤ Aircraft design - Aircraft models - Dynamic models - Flight characteristics - Maneuverability - Modal response - SR-71 aircraft - Structural design criteria - Vibration simulators
Edition Identifiers:
- The Open Library ID: OL17593996M - OL15504630M
- Online Computer Library Center (OCLC) ID: 40451058
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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6Electromagnetic on-aircraft antenna radiation in the presence of composite plates
By S. H-T Kan
“Electromagnetic on-aircraft antenna radiation in the presence of composite plates” Metadata:
- Title: ➤ Electromagnetic on-aircraft antenna radiation in the presence of composite plates
- Author: S. H-T Kan
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center - The Ohio State University, ElectroScience Laboratory, Dept. of Electrical Engineering
- Publish Date: 1994
- Publish Location: ➤ Columbus, Ohio - Springfield, Va - Hampton, VA
“Electromagnetic on-aircraft antenna radiation in the presence of composite plates” Subjects and Themes:
- Subjects: ➤ Aircraft antennas - Aircraft models - Antenna radiation patterns - Composite structures - Electrical impedance - Electromagnetic radiation - Electromagnetic scattering - Plates (Structural members)
Edition Identifiers:
- The Open Library ID: OL15403639M - OL18076286M - OL17001402M
- Online Computer Library Center (OCLC) ID: 32216791
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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7Development and implementation of software for visualizing and editing multidimensional flight simulation input data
By Todd Michael Whelan
“Development and implementation of software for visualizing and editing multidimensional flight simulation input data” Metadata:
- Title: ➤ Development and implementation of software for visualizing and editing multidimensional flight simulation input data
- Author: Todd Michael Whelan
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Development and implementation of software for visualizing and editing multidimensional flight simulation input data” Subjects and Themes:
- Subjects: Aerodynamic characteristics - Graphical user interface - Aircraft models - Computerized simulation - Windows (Computer programs)
Edition Identifiers:
- The Open Library ID: OL17837370M - OL17697882M
- Online Computer Library Center (OCLC) ID: 40128311
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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8User's manual for interactive LINEAR, a FORTRAN program to derive linear aircraft models
By Robert F. Antoniewicz
“User's manual for interactive LINEAR, a FORTRAN program to derive linear aircraft models” Metadata:
- Title: ➤ User's manual for interactive LINEAR, a FORTRAN program to derive linear aircraft models
- Author: Robert F. Antoniewicz
- Language: English
- Number of Pages: Median: 121
- Publisher: ➤ For sale by the National Technical Information Service] - Ames Research Center - National Aeronautics and Space Administration, Scientific and Technical Information Division
- Publish Date: 1988 - 1989
- Publish Location: ➤ [Springfield, Va - Edwards, Calif - [Washington, DC]
“User's manual for interactive LINEAR, a FORTRAN program to derive linear aircraft models” Subjects and Themes:
- Subjects: ➤ FORTRAN - LINEAR - Computer programs - Linearization - Mathematical models - Aircraft models
Edition Identifiers:
- The Open Library ID: OL15277465M - OL19987194M
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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9High speed civil transport aircraft simulation
By Robert A. Sotack
“High speed civil transport aircraft simulation” Metadata:
- Title: ➤ High speed civil transport aircraft simulation
- Author: Robert A. Sotack
- Language: English
- Publisher: ➤ Available from National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1999
- Publish Location: Hampton, Va - Springfield, VA
“High speed civil transport aircraft simulation” Subjects and Themes:
- Subjects: ➤ Civil aviation - Transport aircraft - Mathematical models - Aircraft models - Algorithms - Boeing aircraft - Supersonic transports - Computerized simulation
Edition Identifiers:
- The Open Library ID: OL15567983M - OL17594992M
- Online Computer Library Center (OCLC) ID: 44115308
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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10Measurements of pressures on the tail and aft fuselage of an airplane model during rotary motions at spin attitudes
By James S. Bowman
“Measurements of pressures on the tail and aft fuselage of an airplane model during rotary motions at spin attitudes” Metadata:
- Title: ➤ Measurements of pressures on the tail and aft fuselage of an airplane model during rotary motions at spin attitudes
- Author: James S. Bowman
- Language: English
- Number of Pages: Median: 82
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - For sale by the National Technical Information Service]
- Publish Date: 1989
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Measurements of pressures on the tail and aft fuselage of an airplane model during rotary motions at spin attitudes” Subjects and Themes:
- Subjects: ➤ Statistics - Measurement - Fuselages - Spin (Aerodynamics) - Pressure measurement - Aircraft models - Airplanes - Pressure - Spin tests - Fuselage - Tail assemblies - Aerodynamic load
Edition Identifiers:
- The Open Library ID: OL16137794M
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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11Effects of yaw and pitch motion on model attitude measurements
By Ping Tcheng
“Effects of yaw and pitch motion on model attitude measurements” Metadata:
- Title: ➤ Effects of yaw and pitch motion on model attitude measurements
- Author: Ping Tcheng
- 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
“Effects of yaw and pitch motion on model attitude measurements” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Dynamic response - Angular velocity - Mathematical models - Wind tunnel tests - Aircraft models - Dimensional measurement - Pitching moments - Yaw
Edition Identifiers:
- The Open Library ID: OL17788772M - OL15410962M
- Online Computer Library Center (OCLC) ID: 32864042
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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12Integrated Advanced Microwave Sounding Unit-A (AMSU-A), performance verification report, METSAT Phase Locked Oscillator assembly, P/N 1348360-1, S/N's F07 and F08
By D. Pines
“Integrated Advanced Microwave Sounding Unit-A (AMSU-A), performance verification report, METSAT Phase Locked Oscillator assembly, P/N 1348360-1, S/N's F07 and F08” Metadata:
- Title: ➤ Integrated Advanced Microwave Sounding Unit-A (AMSU-A), performance verification report, METSAT Phase Locked Oscillator assembly, P/N 1348360-1, S/N's F07 and F08
- Author: D. Pines
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Integrated Advanced Microwave Sounding Unit-A (AMSU-A), performance verification report, METSAT Phase Locked Oscillator assembly, P/N 1348360-1, S/N's F07 and F08” Subjects and Themes:
- Subjects: ➤ Advanced Microwave Sounding Unit - Aircraft models - Oscillators - Performance tests - Thermal cycling tests - Vibration
Edition Identifiers:
- The Open Library ID: OL17584198M - OL15550669M
- Online Computer Library Center (OCLC) ID: 42289497
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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13Acoustic and aerodynamic study of a pusher-propeller aircraft model
By Paul T. Soderman
“Acoustic and aerodynamic study of a pusher-propeller aircraft model” Metadata:
- Title: ➤ Acoustic and aerodynamic study of a pusher-propeller aircraft model
- Author: Paul T. Soderman
- 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: ➤ Springfield, Va - [Washington, D.C.]
“Acoustic and aerodynamic study of a pusher-propeller aircraft model” Subjects and Themes:
- Subjects: ➤ Aerial Propellers - Aeroacoustics - Aircraft models - Aircraft wakes - Interactional aerodynamics - Noise - Propeller blades - Propeller noise - Wakes (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL16135237M
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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14Controls design with crossfeeds for hovering rotcract using quantitative feedback theory
By Daniel J. Biezad
“Controls design with crossfeeds for hovering rotcract using quantitative feedback theory” Metadata:
- Title: ➤ Controls design with crossfeeds for hovering rotcract using quantitative feedback theory
- Author: Daniel J. Biezad
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Controls design with crossfeeds for hovering rotcract using quantitative feedback theory” Subjects and Themes:
- Subjects: ➤ Aircraft models - Directional stability - Dynamic response - Feedback - Flight control - Flight simulation - Helicopter control - Hovering stability - Rotary wing aircraft
Edition Identifiers:
- The Open Library ID: OL15417394M
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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15Controls design with crossfeeds for hovering rotorcraft using quantitative feedback theory
By Daniel J. Biezad
“Controls design with crossfeeds for hovering rotorcraft using quantitative feedback theory” Metadata:
- Title: ➤ Controls design with crossfeeds for hovering rotorcraft using quantitative feedback theory
- Author: Daniel J. Biezad
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Controls design with crossfeeds for hovering rotorcraft using quantitative feedback theory” Subjects and Themes:
- Subjects: ➤ Aircraft models - Directional stability - Dynamic response - Feedback - Flight control - Flight simulation - Helicopter control - Hovering stability - Rotary wing aircraft
Edition Identifiers:
- The Open Library ID: OL17792124M
- Online Computer Library Center (OCLC) ID: 33395180
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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16Computer-automated opponent for manned air-to-air combat simulations
By Walter W. Hankins
“Computer-automated opponent for manned air-to-air combat simulations” Metadata:
- Title: ➤ Computer-automated opponent for manned air-to-air combat simulations
- Author: Walter W. Hankins
- Language: English
- Number of Pages: Median: 150
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1979
- Publish Location: Washington, D.C
“Computer-automated opponent for manned air-to-air combat simulations” Subjects and Themes:
- Subjects: ➤ Military Airplanes - Combat - Data processing - Computerized simulation - Fighter aircraft - Aircraft models - Automatic control
Edition Identifiers:
- The Open Library ID: OL43506460M
- Online Computer Library Center (OCLC) ID: 761249743
Access and General Info:
- First Year Published: 1979
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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17Specimen designs for testing advanced aeropropulsion materials under in-plane biaxial loading
By Ellis, John R.
“Specimen designs for testing advanced aeropropulsion materials under in-plane biaxial loading” Metadata:
- Title: ➤ Specimen designs for testing advanced aeropropulsion materials under in-plane biaxial loading
- Author: Ellis, John R.
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 2003
- Publish Location: [Cleveland, Ohio]
“Specimen designs for testing advanced aeropropulsion materials under in-plane biaxial loading” Subjects and Themes:
- Subjects: ➤ Aerodynamic loads - Aircraft models - Fatigue (Materials) - Loads (Forces) - Materials selection - Stress analysis - Stress cycles - Structural design criteria
Edition Identifiers:
- The Open Library ID: OL16094089M
Access and General Info:
- First Year Published: 2003
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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18A method for landing gear modeling and simulation with experimental validation
By James N. Daniels
“A method for landing gear modeling and simulation with experimental validation” Metadata:
- Title: ➤ A method for landing gear modeling and simulation with experimental validation
- Author: James N. Daniels
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: Hampton, Va - [Springfield, Va
“A method for landing gear modeling and simulation with experimental validation” Subjects and Themes:
- Subjects: ➤ Landing gear - Aircraft models - Computerized simulation - Nonlinearity - Vibration - Aircraft landing - Landing simulation - Equations of motion
Edition Identifiers:
- The Open Library ID: OL15452328M
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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19Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane
By Dennis O. Allison
“Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane” Metadata:
- Title: ➤ Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane
- Author: Dennis O. Allison
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service (NTIS) [distributor
- Publish Date: 1995
- Publish Location: Springfield, VA - Hampton, Va
“Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane” Subjects and Themes:
- Subjects: ➤ Pressure distribution - Wind tunnel tests - Aircraft models - Subsonic speed - Transonic speed - Maneuverability - Trailing edges - Airfoils - Wing-fuselage stores - Leading edges
Edition Identifiers:
- The Open Library ID: OL15413576M
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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20Simplified aerodynamic and structural modeling for oblique all-wing aircraft--phase 2: structures
By Ilan Kroo
“Simplified aerodynamic and structural modeling for oblique all-wing aircraft--phase 2: structures” Metadata:
- Title: ➤ Simplified aerodynamic and structural modeling for oblique all-wing aircraft--phase 2: structures
- Author: Ilan Kroo
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1994
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Simplified aerodynamic and structural modeling for oblique all-wing aircraft--phase 2: structures” Subjects and Themes:
- Subjects: Oblique wings - Aircraft design - Tailless aircraft - Predictions - Aircraft models
Edition Identifiers:
- The Open Library ID: OL15481341M
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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21Nonlinear axisymmetric and three-dimensional vorticity dynamics in a swirling jet model
By J. E. Martin
“Nonlinear axisymmetric and three-dimensional vorticity dynamics in a swirling jet model” Metadata:
- Title: ➤ Nonlinear axisymmetric and three-dimensional vorticity dynamics in a swirling jet model
- Author: J. E. Martin
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - Institute for Computer Applications in Science and Engineering, NASA Langley Research Center
- Publish Date: 1996
- Publish Location: [Springfield, Va - Hampton, VA
“Nonlinear axisymmetric and three-dimensional vorticity dynamics in a swirling jet model” Subjects and Themes:
- Subjects: Computational fluid dynamics - Aircraft models - Three dimensional motion - Vorticity - Swirling
Edition Identifiers:
- The Open Library ID: OL15504912M
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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22Generic airplane model concept and four specific models developed for use in piloted simulation studies
By Keith D. Hoffler
“Generic airplane model concept and four specific models developed for use in piloted simulation studies” Metadata:
- Title: ➤ Generic airplane model concept and four specific models developed for use in piloted simulation studies
- Author: Keith D. Hoffler
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: [Springfield, Va - Hampton, Va
“Generic airplane model concept and four specific models developed for use in piloted simulation studies” Subjects and Themes:
- Subjects: ➤ Flight envelopes - Controllability - Flight control - Flight optimization - Flight simulation - Aircraft models
Edition Identifiers:
- The Open Library ID: OL15487239M
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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23A verification procedure for MSC/NASTRAN finite element models
By Alan E. Stockwell
“A verification procedure for MSC/NASTRAN finite element models” Metadata:
- Title: ➤ A verification procedure for MSC/NASTRAN finite element models
- Author: Alan E. Stockwell
- 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
“A verification procedure for MSC/NASTRAN finite element models” Subjects and Themes:
- Subjects: ➤ Aircraft structures - Finite element method - Mathematical models - Aircraft models - Program verification (Computers) - Design analysis
Edition Identifiers:
- The Open Library ID: OL15413626M
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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24Lateral stability analysis for X-29A drop model using system identification methodology
By David L. Raney
“Lateral stability analysis for X-29A drop model using system identification methodology” Metadata:
- Title: ➤ Lateral stability analysis for X-29A drop model using system identification methodology
- Author: David L. Raney
- Language: English
- Number of Pages: Median: 24
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - For sale by the National Technical Information Service]
- Publish Date: 1989
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Lateral stability analysis for X-29A drop model using system identification methodology” Subjects and Themes:
- Subjects: ➤ Aircraft models - Directional stability - Drop tests - Flight characteristics - Flight stability tests - Grumman X-29A (Jet plane) - Lateral Stability of airplanes - Lateral stability - Measurement - Stability of airplanes, Lateral - Swept forward wings - System identification - X-29 aircraft
Edition Identifiers:
- The Open Library ID: OL17683289M
Access and General Info:
- First Year Published: 1989
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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25Numerical stability and control analysis towards falling-leaf prediction capabilities of splitflow for two generic high-performance aircraft models
By Eric F. Charlton
“Numerical stability and control analysis towards falling-leaf prediction capabilities of splitflow for two generic high-performance aircraft models” Metadata:
- Title: ➤ Numerical stability and control analysis towards falling-leaf prediction capabilities of splitflow for two generic high-performance aircraft models
- Author: Eric F. Charlton
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1998
- Publish Location: Hampton, Va - Springfield, VA
“Numerical stability and control analysis towards falling-leaf prediction capabilities of splitflow for two generic high-performance aircraft models” Subjects and Themes:
- Subjects: ➤ Aircraft performance - Computational fluid dynamics - Supersonic aircraft - Aircraft models - Design analysis - Angle of attack - Aerodynamic characteristics - Fighter aircraft
Edition Identifiers:
- The Open Library ID: OL15547010M
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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26NASA Dryden Flow Visualization Facility
By John H. Del Frate
“NASA Dryden Flow Visualization Facility” Metadata:
- Title: ➤ NASA Dryden Flow Visualization Facility
- Author: John H. Del Frate
- Language: English
- Publisher: ➤ National Technical Information Service, distributor] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“NASA Dryden Flow Visualization Facility” Subjects and Themes:
- Subjects: ➤ Light beams - Data correlation - Shadowgraph photography - Reynolds number - Aircraft models - Laser outputs
Edition Identifiers:
- The Open Library ID: OL15413441M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
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27A Modified lifted line theory for wing-propeller interference
By R. K. Prabhu
“A Modified lifted line theory for wing-propeller interference” Metadata:
- Title: ➤ A Modified lifted line theory for wing-propeller interference
- Author: R. K. Prabhu
- Language: English
- Publisher: ➤ Old Dominion University Research Foundation
- Publish Date: 1983
- Publish Location: Norfolk, Va
“A Modified lifted line theory for wing-propeller interference” Subjects and Themes:
- Subjects: ➤ Aerial Propellers - Aircraft models - Airfoils - Airplanes - Efficiency - Incompressible flow - Interference (Aerodynamics) - Inviscid flow - Lifting bodies - Perturbation - Propeller slipstreams - Propellers, Aerial - Research - Wings
Edition Identifiers:
- The Open Library ID: OL16153779M
Access and General Info:
- First Year Published: 1983
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
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28Automation of reverse engineering process in aircraft modeling and related optimization problems
By W. Li
“Automation of reverse engineering process in aircraft modeling and related optimization problems” Metadata:
- Title: ➤ Automation of reverse engineering process in aircraft modeling and related optimization problems
- Author: W. Li
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - Old Dominion Research Foundation
- Publish Date: 1994
- Publish Location: ➤ [Washington, DC - Springfield, Va - Norfolk, VA
“Automation of reverse engineering process in aircraft modeling and related optimization problems” Subjects and Themes:
- Subjects: ➤ Reverse engineering - Aircraft design - Data processing - Aircraft parts - Aerodynamic configurations - Aircraft models - Quadratic programming
Edition Identifiers:
- The Open Library ID: OL15408849M
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
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29An investigation of helicopter dynamic coupling using an analytical model
By Jeffrey D. Keller
“An investigation of helicopter dynamic coupling using an analytical model” Metadata:
- Title: ➤ An investigation of helicopter dynamic coupling using an analytical model
- Author: Jeffrey D. Keller
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va
“An investigation of helicopter dynamic coupling using an analytical model” Subjects and Themes:
- Subjects: Helicopters - Aircraft models - Rotor body interactions - Helicopter control - Mathematical models
Edition Identifiers:
- The Open Library ID: OL15410322M
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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30An evaluation technique for an F/A-18 aircraft loads model using F/A-18 systems research aircraft flight data
By Marty Brenner
“An evaluation technique for an F/A-18 aircraft loads model using F/A-18 systems research aircraft flight data” Metadata:
- Title: ➤ An evaluation technique for an F/A-18 aircraft loads model using F/A-18 systems research aircraft flight data
- Author: Marty Brenner
- Language: English
- Publisher: ➤ Available from NASA Center for AeroSpace Information (CASI) - National Aeronautics and Space Administration, Dryden Flight Research Center
- Publish Date: 2000
- Publish Location: Edwards, Calif - Hanover, MD
“An evaluation technique for an F/A-18 aircraft loads model using F/A-18 systems research aircraft flight data” Subjects and Themes:
- Subjects: ➤ F-18 aircraft - Flight conditions - Aeroelasticity - Aircraft models - Wing loading - Flight simulators - Flight tests
Edition Identifiers:
- The Open Library ID: OL16036973M
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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31Activity tracking for pilot error detection from flight data
By Todd J. Callantine
“Activity tracking for pilot error detection from flight data” Metadata:
- Title: ➤ Activity tracking for pilot error detection from flight data
- Author: Todd J. Callantine
- Language: English
- Publisher: ➤ National Aeronautcs and Space Administration, Ames Research Center - For sale by the National Technical Information Service
- Publish Date: 2002
- Publish Location: ➤ [Springfield, Va - Moffett Field, CA
“Activity tracking for pilot error detection from flight data” Subjects and Themes:
- Subjects: ➤ Flight crews - Detection - Boeing 757 aircraft - Aircraft models - Data acquisition - Pilot error
Edition Identifiers:
- The Open Library ID: OL16125363M
Access and General Info:
- First Year Published: 2002
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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