Study of V/STOL Aircraft Implementation. Volume 2: Appendices
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Published: 1972
Total Pages: 392
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Author:
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Published: 1972
Total Pages: 392
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Published: 1973
Total Pages: 98
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DOWNLOAD EBOOKAuthor: W.J. Portenier
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Published: 1973
Total Pages:
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DOWNLOAD EBOOKAuthor:
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Published: 1973
Total Pages: 102
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DOWNLOAD EBOOKAuthor: W. J. Portenier
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Published: 1973
Total Pages: 82
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Published: 1973
Total Pages:
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DOWNLOAD EBOOKAuthor: James A. Franklin
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Published: 2000
Total Pages: 198
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DOWNLOAD EBOOKThis publication presents materials that constituted the lectures presented by the author as part of Course AA 234 Dynamics, Control, and Flying Qualities of V/STOL Aircraft that was taught in the Department of Aeronautics and Astronautics at Stanford University. It covers representative operations of vertical and short takeoff and landing (V/STOL) aircraft, a discussion of the pilot's strategy in controlling these aircraft, the equations of motion pertinent to V/STOL tasks, and their application in the analysis of longitudinal and lateral-directional control in hover and forward flight. Following that development, which applies to the characteristics of the basic airframe and propulsion system, the text concludes with a discussion of the contributions of control augmentation in specific flight tasks and of the integration of modern electronic displays with these controls.
Author: K. Clark White
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Published: 1985
Total Pages: 20
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DOWNLOAD EBOOKAuthor: Seth B. Anderson
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Published: 1960
Total Pages: 56
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DOWNLOAD EBOOKA study has been undertaken to define hand-ling qualities criteria for V/STOL aircraft. With the current military requirements for helicopters and airplanes as a framework, modifications and additions were made for conversion to a preliminary set of V/STOL requirements using a broad background of flight experience and pilots' comments from VTOL and STOL aircraft, BLC (boundary-layer-control) equipped aircraft, variable stability aircraft, flight simulators and landing approach studies. The report contains a discussion of the reasoning behind and the sources of information leading to suggested requirements. The results of the study indicate that the majority of V/STOL requirements can be defined by modifications to the helicopter and/or airplane requirements by appropriate definition of reference speeds. Areas where a requirement is included but where the information is felt to be inadequate to establish a firm quantitative requirement include the following: Control power and damping relationships about all axes for various sizes and types of aircraft; control power, sensitivity, d-amping and response for height control; dynamic longitudinal and dynamic lateral- directional stability in the transition region, including emergency operation; hovering steadiness; acceleration and deceleration in transition; descent rates and flight-path angles in steep approaches, and thrust margin for approach.
Author: Ling-Temco-Vought
Publisher:
Published: 1967
Total Pages: 116
ISBN-13:
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