Introduction to V/STOL Airplanes PDF Download
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Author: David L. Kohlman
Publisher: Wiley-Blackwell
ISBN:
Category : Transportation
Languages : en
Pages : 252
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Book Description
Author: David L. Kohlman
Publisher: Wiley-Blackwell
ISBN:
Category : Transportation
Languages : en
Pages : 252
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Book Description
Author: Franklin D. Harris
Publisher:
ISBN: 9780692568309
Category : Autogiros
Languages : en
Pages : 797
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Book Description
Author: Barnes Warnock McCormick
Publisher: Courier Corporation
ISBN: 9780486404608
Category : Technology & Engineering
Languages : en
Pages : 356
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Book Description
An extremely practical overview of V/STOL (vertical/short takeoff and landing) aerodynamics, this volume offers a presentation of general theoretical and applied aerodynamic principles, covering propeller and helicopter rotor theory for both the static and forward flight cases. Both a text for students and a reference for professionals, the book can be used for advanced undergraduate or graduate courses. Numerous detailed figures, plus exercises. 1967 edition. Preface. Appendix. Index.
Author: Franklin D. Harris
Publisher:
ISBN:
Category : Autogiros
Languages : en
Pages :
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Book Description
Author:
Publisher:
ISBN:
Category : Short take-off and landing aircraft
Languages : en
Pages : 8
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Book Description
Author: David L. Kohlman
Publisher: Wiley-Blackwell
ISBN:
Category : Transportation
Languages : en
Pages : 252
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Book Description
Author: Franklin D. Harris
Publisher:
ISBN: 9780615715629
Category : Autogiros
Languages : en
Pages :
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Book Description
Author: Franklin D. Harris
Publisher:
ISBN:
Category : Autogiros
Languages : en
Pages :
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Book Description
Author: J. R. Nelson
Publisher:
ISBN:
Category : History
Languages : en
Pages : 52
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Book Description
As aeronautical technologies continue to advance, V/STOL airplanes will become increasingly more attractive for a variety of military missions. The decision whether to approve the acquisition of a V/STOL airplane for a particular mission will depend upon factors that include the airplane's expected performance capability, the likely acquisition cost, and the likely amount of time required for research and development. To develop guidelines and techniques for critically evaluating these factors, RAND has analyzed past V/STOL research and development programs, examined the current state of pertinent aeronautical technologies, and developed appropriate analytical tools where suitable information exists. The introduction of future V/STOL airplanes for military missions will continue to depend on mission needs that place a high operational value on the special capabilities of V/STOL airplanes--an operational value high enough to warrant the exceptionally long development times and the premium prices (compared with conventional airplanes) that must be paid for research, development, and procurement.
Author: Seth B. Anderson
Publisher:
ISBN:
Category : Flight control
Languages : en
Pages : 56
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Book Description
A 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.
