Explore: Aircraft Stability
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Source: The Open Library
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1Flight stability and automatic control
By Robert C. Nelson
“Flight stability and automatic control” Metadata:
- Title: ➤ Flight stability and automatic control
- Author: Robert C. Nelson
- Language: English
- Number of Pages: Median: 363
- Publisher: McGraw-Hill - WCB/McGraw Hill
- Publish Date: 1989 - 1998
- Publish Location: New York - Boston, Mass
“Flight stability and automatic control” Subjects and Themes:
- Subjects: ➤ Airplanes - Control systems - Automatic control - Stability of airplanes - Airplanes, control systems - Aeronaves - Estabilidade de vôo - Controle automático - Aircraft stability - Flight control - Aircraft control - Textbooks
Edition Identifiers:
- The Open Library ID: OL2402207M - OL679598M
- Online Computer Library Center (OCLC) ID: 37179622 - 17106068
- Library of Congress Control Number (LCCN): 87032481 - 97026109
- All ISBNs: 9780070462731 - 0070462186 - 9780070462182 - 0070462739
Access and General Info:
- First Year Published: 1989
- Is Full Text Available: Yes
- Is The Book Public: No
- Access Status: Printdisabled
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2Launch vehicle flight dynamics
By John E. Cochran
“Launch vehicle flight dynamics” Metadata:
- Title: Launch vehicle flight dynamics
- Author: John E. Cochran
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Launch vehicle flight dynamics” Subjects and Themes:
- Subjects: Aerodynamic characteristics - Aircraft stability - Flight control - Launch vehicles - Payloads
Edition Identifiers:
- The Open Library ID: OL17796471M - OL15423103M
- Online Computer Library Center (OCLC) ID: 35246468
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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3Estimation of aircraft nonlinear unsteady parameters from wind tunnel data
By Vladislav Klein
“Estimation of aircraft nonlinear unsteady parameters from wind tunnel data” Metadata:
- Title: ➤ Estimation of aircraft nonlinear unsteady parameters from wind tunnel data
- Author: Vladislav Klein
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: Hampton, Va - [Springfield, Va
“Estimation of aircraft nonlinear unsteady parameters from wind tunnel data” Subjects and Themes:
- Subjects: ➤ Aerodynamic forces - Aircraft stability - Flight stability tests - Mathematical models - Unsteady aerodynamics - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL17839051M - OL15542530M
- Online Computer Library Center (OCLC) ID: 41469910
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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4Cooperative control theory and integrated flight and propulsion control
By D. K. Schmidt
“Cooperative control theory and integrated flight and propulsion control” Metadata:
- Title: ➤ Cooperative control theory and integrated flight and propulsion control
- Author: D. K. Schmidt
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - Dept. of Aerospace Engineering, University of Maryland - National Aeronautics and Space Administration
- Publish Date: 1994 - 1995
- Publish Location: ➤ Springfield, Va - [Washington, DC - College Park, Md
“Cooperative control theory and integrated flight and propulsion control” Subjects and Themes:
- Subjects: ➤ Aircraft design - Aircraft stability - Airframes - Control systems design - Control theory - Controllability - Engine airframe integration - Engine control - Feedback control - Propulsion - Propulsion system performance - STOVL aircraft - Systems analysis - Systems engineering - V/STOL aircraft
Edition Identifiers:
- The Open Library ID: OL15408544M - OL15418914M
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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5Bibliography for aircraft parameter estimation
By Kenneth W. Iliff
“Bibliography for aircraft parameter estimation” Metadata:
- Title: ➤ Bibliography for aircraft parameter estimation
- Author: Kenneth W. Iliff
- Language: English
- Number of Pages: Median: 18
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service] - Dryden Flight Research Facility
- Publish Date: 1986 - 1987
- Publish Location: ➤ [Washington, DC] - Edwards, Calif - [Springfield, Va
“Bibliography for aircraft parameter estimation” Subjects and Themes:
- Subjects: ➤ Aircraft control - Aircraft stability - Airplanes - Bibliography - Flight testing - Flight tests - Parameter estimation
Edition Identifiers:
- The Open Library ID: OL15288182M - OL20984977M
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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6Determining the accuracy of maximum likelihood parameter estimates with colored residuals
By Eugene A. Morelli
“Determining the accuracy of maximum likelihood parameter estimates with colored residuals” Metadata:
- Title: ➤ Determining the accuracy of maximum likelihood parameter estimates with colored residuals
- Author: Eugene A. Morelli
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: Hampton, Va - [Springfield, Va
“Determining the accuracy of maximum likelihood parameter estimates with colored residuals” Subjects and Themes:
- Subjects: Aircraft stability - Dynamic characteristics - Mathematical models - Maximum likelihood estimates - Parameter identification
Edition Identifiers:
- The Open Library ID: OL15403780M
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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7Synthesis from design requirements of a hybrid system for transport aircraft longitudinal control
By Charles S. Hynes
“Synthesis from design requirements of a hybrid system for transport aircraft longitudinal control” Metadata:
- Title: ➤ Synthesis from design requirements of a hybrid system for transport aircraft longitudinal control
- Author: Charles S. Hynes
- Language: English
- Publisher: ➤ National Aeronautics and, Space Administration, Ames Research Center
- Publish Date: 2007
- Publish Location: Moffett Field, Calif
“Synthesis from design requirements of a hybrid system for transport aircraft longitudinal control” Subjects and Themes:
- Subjects: ➤ Avionics - Transport aircraft - Aircraft stability - Systems engineering - Dynamical systems - Flight management systems - Systems analysis - Automatic pilots - Longitudinal control - Mathematical models - Aerodynamic characteristics - Aircraft performance - Requirements
Edition Identifiers:
- The Open Library ID: OL53682026M
- Online Computer Library Center (OCLC) ID: 826145520
Access and General Info:
- First Year Published: 2007
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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8Initial evaluation of the modified stepwise regression procedure to estimate aircraft stability and control parameters from flight test data
By J. C. Hoff
“Initial evaluation of the modified stepwise regression procedure to estimate aircraft stability and control parameters from flight test data” Metadata:
- Title: ➤ Initial evaluation of the modified stepwise regression procedure to estimate aircraft stability and control parameters from flight test data
- Author: J. C. Hoff
- Number of Pages: Median: 41
- Publisher: ➤ Cranfield University, College of Aeronautics
- Publish Date: 1993
- Publish Location: Cranfield, Bedford, England\
“Initial evaluation of the modified stepwise regression procedure to estimate aircraft stability and control parameters from flight test data” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL19754127M
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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9Application of parameter estimation to highly unstable aircraft
By Richard E. Maine
“Application of parameter estimation to highly unstable aircraft” Metadata:
- Title: ➤ Application of parameter estimation to highly unstable aircraft
- Author: Richard E. Maine
- Language: English
- Number of Pages: Median: 11
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility - For sale by the National Technical Information Service]
- Publish Date: 1986
- Publish Location: ➤ [Springfield, Va - Edwards, Calif
“Application of parameter estimation to highly unstable aircraft” Subjects and Themes:
- Subjects: Aircraft stability - Error analysis - Flight tests - Parameter estimation - Systems stability
Edition Identifiers:
- The Open Library ID: OL17115153M
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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10Measurement of the longitudinal static stability and the moments of 0inertia of a 1/12th scale model of a B.Ae Hawk
By H. A. Hinds
“Measurement of the longitudinal static stability and the moments of 0inertia of a 1/12th scale model of a B.Ae Hawk” Metadata:
- Title: ➤ Measurement of the longitudinal static stability and the moments of 0inertia of a 1/12th scale model of a B.Ae Hawk
- Author: H. A. Hinds
- Publisher: ➤ College of Aeronautics, Cranfield Institute of Technology
- Publish Date: 1990
- Publish Location: Cranfield, Bedford
“Measurement of the longitudinal static stability and the moments of 0inertia of a 1/12th scale model of a B.Ae Hawk” Subjects and Themes:
- Subjects: Aircraft control - Aircraft stability - Stepwise regression
Edition Identifiers:
- The Open Library ID: OL19167531M
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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11Review of initial experiments using the Hawk model, dynamic rig facility and the CED1401 digital data acquisition equipment
By H. A. Hinds
“Review of initial experiments using the Hawk model, dynamic rig facility and the CED1401 digital data acquisition equipment” Metadata:
- Title: ➤ Review of initial experiments using the Hawk model, dynamic rig facility and the CED1401 digital data acquisition equipment
- Author: H. A. Hinds
- Number of Pages: Median: 27
- Publisher: ➤ Cranfield Institute of Technology, College of Aeronautics
- Publish Date: 1990
- Publish Location: Cranfield, Bedford, England
“Review of initial experiments using the Hawk model, dynamic rig facility and the CED1401 digital data acquisition equipment” Subjects and Themes:
- Subjects: Aircraft control - Aircraft stability - Stepwise regression
Edition Identifiers:
- The Open Library ID: OL19246964M
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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12Second quarterly report on the application of modified stepwise regression for the estimation of aircraft stability and control parameters
By H. A. Hinds
“Second quarterly report on the application of modified stepwise regression for the estimation of aircraft stability and control parameters” Metadata:
- Title: ➤ Second quarterly report on the application of modified stepwise regression for the estimation of aircraft stability and control parameters
- Author: H. A. Hinds
- Number of Pages: Median: 46
- Publisher: ➤ Cranfield Institute of Technology, College of Aeronautics
- Publish Date: 1989
- Publish Location: Cranfield, Bedford, England
“Second quarterly report on the application of modified stepwise regression for the estimation of aircraft stability and control parameters” Subjects and Themes:
- Subjects: Aircraft control - Aircraft stability
Edition Identifiers:
- The Open Library ID: OL20966695M
- All ISBNs: 1871315034 - 9781871315035
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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13Third quarterly report on the application of modified stepwise regression for the estimation of aircraft stability and control parameters
By H. A. Hinds
“Third quarterly report on the application of modified stepwise regression for the estimation of aircraft stability and control parameters” Metadata:
- Title: ➤ Third quarterly report on the application of modified stepwise regression for the estimation of aircraft stability and control parameters
- Author: H. A. Hinds
- Number of Pages: Median: 34
- Publisher: ➤ College of Aeronautics, Cranfield Institute of Technology
- Publish Date: 1989
- Publish Location: Cranfield, Bedford
“Third quarterly report on the application of modified stepwise regression for the estimation of aircraft stability and control parameters” Subjects and Themes:
- Subjects: Aircraft control - Aircraft stability - Stepwise regression
Edition Identifiers:
- The Open Library ID: OL19167566M
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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14Aerodynamic stability and control data, model 844-2035
By Boeing Company
“Aerodynamic stability and control data, model 844-2035” Metadata:
- Title: ➤ Aerodynamic stability and control data, model 844-2035
- Author: Boeing Company
- Number of Pages: Median: 194
- Publisher: Boeing Company
- Publish Date: 1972
- Publish Location: Seattle, Wash
“Aerodynamic stability and control data, model 844-2035” Subjects and Themes:
- Subjects: Aircraft stability - Aircraft control
Edition Identifiers:
- The Open Library ID: OL21499490M
Access and General Info:
- First Year Published: 1972
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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15Relative control effectiveness technique with application to airplane control coordination
By Frederick J. Lallman
“Relative control effectiveness technique with application to airplane control coordination” Metadata:
- Title: ➤ Relative control effectiveness technique with application to airplane control coordination
- Author: Frederick J. Lallman
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service,] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1985
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Relative control effectiveness technique with application to airplane control coordination” Subjects and Themes:
- Subjects: ➤ Aircraft control - Aircraft stability - Airplanes - Control systems - Directional control - Lateral Stability of airplanes - Lateral control - Linear systems - Mathematical models - Mathematical optimization - Optimization - Stability of airplanes, Lateral - Thrust vector control
Edition Identifiers:
- The Open Library ID: OL16115007M
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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16Flying qualities handbook
By USAF Test Pilot School
“Flying qualities handbook” Metadata:
- Title: Flying qualities handbook
- Author: USAF Test Pilot School
- Publisher: ➤ USAF Test Pilot School, Air Force Flight Test Center
- Publish Date: 1979
- Publish Location: Edwards AFB, Calif
“Flying qualities handbook” Subjects and Themes:
- Subjects: Flight tests - Gyration - Aircraft control - Aircraft stability
Edition Identifiers:
- The Open Library ID: OL19044257M
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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17PREDAVOR
By Danielle Suzanne Soban
“PREDAVOR” Metadata:
- Title: PREDAVOR
- Author: Danielle Suzanne Soban
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Washington, DC - Springfield, Va
“PREDAVOR” Subjects and Themes:
- Subjects: ➤ Aircraft stability - Controllability - Computer aided design - Computer programs - Stability derivatives - Aircraft design - Flight characteristics
Edition Identifiers:
- The Open Library ID: OL15487258M
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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18Semi-annual status report on NASA grant NAG 1-837, "Aerodynamics of thrust vectoring"
By Jing-Biau Tseng
“Semi-annual status report on NASA grant NAG 1-837, "Aerodynamics of thrust vectoring"” Metadata:
- Title: ➤ Semi-annual status report on NASA grant NAG 1-837, "Aerodynamics of thrust vectoring"
- Author: Jing-Biau Tseng
- Language: English
- Publisher: ➤ Flight Research Laboratory, University of Kansas Center for Research - National Aeronautics and Space Administration
- Publish Date: 1989
- Publish Location: ➤ [Washington, D.C - Lawrence, Kan
“Semi-annual status report on NASA grant NAG 1-837, "Aerodynamics of thrust vectoring"” Subjects and Themes:
- Subjects: Aircraft stability - Attitude control - Thrust vector control - Nozzle thrust coefficients - Aircraft control
Edition Identifiers:
- The Open Library ID: OL16138003M
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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19An aerodynamic tradeoff study of the scissor wing configuration
By Bruce P. Selberg
“An aerodynamic tradeoff study of the scissor wing configuration” Metadata:
- Title: ➤ An aerodynamic tradeoff study of the scissor wing configuration
- Author: Bruce P. Selberg
- Language: English
- Publisher: ➤ University of Missouri-Rolla - National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1990
- Publish Location: ➤ Springfield, Va - [Hampton, Va - Rolla, Mo
“An aerodynamic tradeoff study of the scissor wing configuration” Subjects and Themes:
- Subjects: ➤ Aerodynamic coefficients - Lift drag ratio - Design and construction - Aircraft stability - Supersonic flight - Aerofoils - Aerodynamic configurations - Variable sweep wings
Edition Identifiers:
- The Open Library ID: OL16128718M
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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20A historical overview of flight flutter testing
By M. W. Kehoe
“A historical overview of flight flutter testing” Metadata:
- Title: ➤ A historical overview of flight flutter testing
- Author: M. W. Kehoe
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“A historical overview of flight flutter testing” Subjects and Themes:
- Subjects: ➤ Aircraft stability - Flutter analysis histories - Excitation - Experiment design - Unsteady aerodynamics - Procedures - Dynamic structural analysis
Edition Identifiers:
- The Open Library ID: OL16125631M
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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21Estimation of longitudinal stability and control derivatives for an icing research aircraft from flight data
By James G. Batterson
“Estimation of longitudinal stability and control derivatives for an icing research aircraft from flight data” Metadata:
- Title: ➤ Estimation of longitudinal stability and control derivatives for an icing research aircraft from flight data
- Author: James G. Batterson
- Number of Pages: Median: 21
- Publisher: Langley Reserach Center
- Publish Date: 1989
- Publish Location: Hampton, Va
“Estimation of longitudinal stability and control derivatives for an icing research aircraft from flight data” Subjects and Themes:
- Subjects: Aircraft stability - Aircraft control - Ice formation
Edition Identifiers:
- The Open Library ID: OL18929982M
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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22Subsonic wing optimization for handling qualities using ACSYNT
By Dani Soban
“Subsonic wing optimization for handling qualities using ACSYNT” Metadata:
- Title: ➤ Subsonic wing optimization for handling qualities using ACSYNT
- Author: Dani Soban
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Subsonic wing optimization for handling qualities using ACSYNT” Subjects and Themes:
- Subjects: ➤ Aircraft stability - Three dimensional models - Applications programs (Computers) - Vortex lattice method - Aerodynamic stability - Computer aided design
Edition Identifiers:
- The Open Library ID: OL15507258M
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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23NASA/FAA Tailplane Icing Program
By Thomas P. Ratvasky
“NASA/FAA Tailplane Icing Program” Metadata:
- Title: ➤ NASA/FAA Tailplane Icing Program
- Author: Thomas P. Ratvasky
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 2000
- Publish Location: ➤ [Springfield, Va - [Cleveland, Ohio]
“NASA/FAA Tailplane Icing Program” Subjects and Themes:
- Subjects: Aircraft icing - Aircraft stability - Flight tests - Horizontal tail surfaces - Leading edges
Edition Identifiers:
- The Open Library ID: OL15569374M
- Online Computer Library Center (OCLC) ID: 44441990
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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24Effects of wing modification on an aircraft's aerodynamic parameters as determined from flight data
By Robert Alan Hess
“Effects of wing modification on an aircraft's aerodynamic parameters as determined from flight data” Metadata:
- Title: ➤ Effects of wing modification on an aircraft's aerodynamic parameters as determined from flight data
- Author: Robert Alan Hess
- Language: English
- Number of Pages: Median: 63
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1986
- Publish Location: Hampton, Va
“Effects of wing modification on an aircraft's aerodynamic parameters as determined from flight data” Subjects and Themes:
- Subjects: ➤ Airplanes - Aerodynamics - Wing profiles - Aircraft stability - Aerodynamic stalling - Leading edges - General aviation aircraft - Wings - Stability of airplanes
Edition Identifiers:
- The Open Library ID: OL16152660M
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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25Aircraft stability and control data
By Gary L. Teper
“Aircraft stability and control data” Metadata:
- Title: ➤ Aircraft stability and control data
- Author: Gary L. Teper
- Number of Pages: Median: 111
- Publisher: Systems Technology Inc
- Publish Date: 1969
- Publish Location: Hawthorne, Calif
“Aircraft stability and control data” Subjects and Themes:
- Subjects: Aircraft stability - Aircraft control
Edition Identifiers:
- The Open Library ID: OL21499486M
Access and General Info:
- First Year Published: 1969
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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26Identification and correlation of the F-4E stall/post-stall aerodynamic stability and control characteristics from existing test data
By Bernard J. Eulrich
“Identification and correlation of the F-4E stall/post-stall aerodynamic stability and control characteristics from existing test data” Metadata:
- Title: ➤ Identification and correlation of the F-4E stall/post-stall aerodynamic stability and control characteristics from existing test data
- Author: Bernard J. Eulrich
- Number of Pages: Median: 328
- Publisher: Calspan Corporation
- Publish Date: 1973
- Publish Location: Buffalo, N. Y
“Identification and correlation of the F-4E stall/post-stall aerodynamic stability and control characteristics from existing test data” Subjects and Themes:
- Subjects: Aircraft stability - Aircraft control
Edition Identifiers:
- The Open Library ID: OL21499596M
Access and General Info:
- First Year Published: 1973
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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27On the lateral instabilities of aircraft due to parametric excitation
By M. Masak
“On the lateral instabilities of aircraft due to parametric excitation” Metadata:
- Title: ➤ On the lateral instabilities of aircraft due to parametric excitation
- Author: M. Masak
- Number of Pages: Median: 38
- Publisher: ➤ Institute for Aerospace Studies
- Publish Date: 1965
- Publish Location: [Downsview, Ont.]
“On the lateral instabilities of aircraft due to parametric excitation” Subjects and Themes:
- Subjects: Aircraft stability - Lateral stability
Edition Identifiers:
- The Open Library ID: OL21038998M
Access and General Info:
- First Year Published: 1965
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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28Longitudinal stability and control characteristics of the Quiet Short-Haul Research Aircraft (QSRA)
By Jack D. Stephenson
“Longitudinal stability and control characteristics of the Quiet Short-Haul Research Aircraft (QSRA)” Metadata:
- Title: ➤ Longitudinal stability and control characteristics of the Quiet Short-Haul Research Aircraft (QSRA)
- Author: Jack D. Stephenson
- Number of Pages: Median: 38
- Publisher: Ames Research Center
- Publish Date: 1989
- Publish Location: Moffett Field, Calif
“Longitudinal stability and control characteristics of the Quiet Short-Haul Research Aircraft (QSRA)” Subjects and Themes:
- Subjects: Aircraft stability - Short takeoff aircraft
Edition Identifiers:
- The Open Library ID: OL19380254M
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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29An investigation of the effect of ballonet motions on tethered-aerostat longitudinal dynamic stability
By J. D. DeLaurier
“An investigation of the effect of ballonet motions on tethered-aerostat longitudinal dynamic stability” Metadata:
- Title: ➤ An investigation of the effect of ballonet motions on tethered-aerostat longitudinal dynamic stability
- Author: J. D. DeLaurier
- Number of Pages: Median: 11
- Publisher: ➤ Institute for Aerospace Studies
- Publish Date: 1977
- Publish Location: [Downsview, Ont.]
“An investigation of the effect of ballonet motions on tethered-aerostat longitudinal dynamic stability” Subjects and Themes:
- Subjects: Aircraft stability - Airships
Edition Identifiers:
- The Open Library ID: OL22344752M
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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30Modification and validation of conceptual design aerodynamic prediction method HASC95 with VTXCHN
By Alan E. Albright
“Modification and validation of conceptual design aerodynamic prediction method HASC95 with VTXCHN” Metadata:
- Title: ➤ Modification and validation of conceptual design aerodynamic prediction method HASC95 with VTXCHN
- Author: Alan E. Albright
- Publisher: Langley Research Center
- Publish Date: 1996
- Publish Location: Hampton, Va
“Modification and validation of conceptual design aerodynamic prediction method HASC95 with VTXCHN” Subjects and Themes:
- Subjects: Aircraft stability - Aircraft control
Edition Identifiers:
- The Open Library ID: OL19006695M
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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31Initial review of research into the application of modified stepwise regression for the estimation of aircraft stability and control parameters
By M. V. Cook
“Initial review of research into the application of modified stepwise regression for the estimation of aircraft stability and control parameters” Metadata:
- Title: ➤ Initial review of research into the application of modified stepwise regression for the estimation of aircraft stability and control parameters
- Author: M. V. Cook
- Number of Pages: Median: 31
- Publisher: ➤ College of Aeronautics, Cranfield Institute of Technology
- Publish Date: 1989
- Publish Location: Cranfield, Bedford
“Initial review of research into the application of modified stepwise regression for the estimation of aircraft stability and control parameters” Subjects and Themes:
- Subjects: Aircraft stability - Aircraft control - Stepwise regression
Edition Identifiers:
- The Open Library ID: OL19167520M
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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