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A Review Of Technologies Applicable To Low Speed Flight Of High Performance Aircraft Investigated In The Langley 14 X 22 Foot Subsonic Tunnel
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Book Synopsis A Review of Technologies Applicable to Low-speed Flight of High-performance Aircraft Investigated in the Langley 14- X 22-foot Subsonic Tunnel by :
Download or read book A Review of Technologies Applicable to Low-speed Flight of High-performance Aircraft Investigated in the Langley 14- X 22-foot Subsonic Tunnel written by and published by . This book was released on 1988 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722144760 Total Pages :94 pages Book Rating :4.1/5 (447 download)
Book Synopsis A Review of Technologies Applicable to Low-Speed Flight of High-Performance Aircraft Investigated in the Langley 14- X 22-Foot Subsonic Tunnel by : National Aeronautics and Space Administration (NASA)
Download or read book A Review of Technologies Applicable to Low-Speed Flight of High-Performance Aircraft Investigated in the Langley 14- X 22-Foot Subsonic Tunnel written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-02 with total page 94 pages. Available in PDF, EPUB and Kindle. Book excerpt: An extensive research program has been underway at the NASA Langley Research Center to define and develop the technologies required for low-speed flight of high-performance aircraft. This 10-year program has placed emphasis on both short takeoff and landing (STOL) and short takeoff and vertical landing (STOVL) operations rather than on regular up and away flight. A series of NASA in-house as well as joint projects have studied various technologies including high lift, vectored thrust, thrust-induced lift, reversed thrust, an alternate method of providing trim and control, and ground effects. These technologies have been investigated on a number of configurations ranging from industry designs for advanced fighter aircraft to generic wing-canard research models. Test conditions have ranged from hover (or static) through transition to wing-borne flight at angles of attack from -5 to 40 deg at representative thrust coefficients. Paulson, John W., Jr. and Quinto, P. Frank and Banks, Daniel W. and Kemmerly, Guy T. and Gatlin, Gregory M. Langley Research Center...
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Book Synopsis A Review of Technologies Applicable to Low-speed Flight of High-performance Aircraft Investigated in the Langley 14- by 22-foot Subsonic Tunnel by :
Download or read book A Review of Technologies Applicable to Low-speed Flight of High-performance Aircraft Investigated in the Langley 14- by 22-foot Subsonic Tunnel written by and published by . This book was released on 1988 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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