Recent Progress in V/STOL Aircraft Technology PDF Download
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Author:
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ISBN:
Category :
Languages : en
Pages : 18
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Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 18
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Author: Leonard Roberts
Publisher:
ISBN:
Category : Short take-off and landing aircraft
Languages : en
Pages : 36
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Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781725577114
Category :
Languages : en
Pages : 34
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Book Description
Progress in vertical and short takeoff and landing (V/STOL) aircraft technology, in particular, during the 1970 to 1980 period at Ames Research Center is discussed. Although only two kinds of V/STOL aircraft (the helicopter and the British direct lift Harrier) have achieved operational maturity, understanding of the technology has vastly improved during this 10 year period. To pursue an aggressive R and D program at a reasonable cost, it was decided to conduct extensive large scale testing in wind tunnel and flight simulation facilities, to develop low cost research aircraft using modified airframes or engines, and to involve other agencies and industry contractors in joint technical and funding arrangements. The STOL investigations include exploring STOL performance using the rotating cylinder flap concept, the augmentor wing, upon initiation of the Quiet Short Haul Research Aircraft program, the upper surface blown flap concept. The VTOL investigations were conducted using a tilt rotor aircraft, resulting in the XV-15 tilt rotor research aircraft. Direct jet lift is now being considered for application to future supersonic fighter aircraft. Roberts, L. and Deckert, W. R. Ames Research Center NASA-TM-84238, A-8896, NAS 1.15:84238 ...
Author: Ramesh K. Agarwal
Publisher: BoD – Books on Demand
ISBN: 9535124811
Category : Technology & Engineering
Languages : en
Pages : 206
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The book describes the recent progress in some engine technologies and active flow control and morphing technologies and in topics related to aeroacoustics and aircraft controllers. Both the researchers and students should find the material useful in their work.
Author: United States. Congress. House. Committee on Armed Services
Publisher:
ISBN:
Category : Short take-off and landing aircraft
Languages : en
Pages : 22
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 456
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Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
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:
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ISBN:
Category :
Languages : en
Pages : 78
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Author: Walter Z. Collings
Publisher:
ISBN:
Category : Aeronautics, Military
Languages : en
Pages : 214
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Author: James A. Franklin
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 198
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Book Description
This 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.