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F A 18 Forebody Vortex Control Volume 1 Static Tests
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Book Synopsis F/A-18 Forebody Vortex Control. Volume 1: Static Tests by :
Download or read book F/A-18 Forebody Vortex Control. Volume 1: Static Tests written by and published by . This book was released on 1994 with total page 188 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis F/A-18 Forebody Vortex Control: Static tests by :
Download or read book F/A-18 Forebody Vortex Control: Static tests written by and published by . This book was released on 1994 with total page 188 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781723052477 Total Pages :184 pages Book Rating :4.0/5 (524 download)
Book Synopsis F/A-18 Forebody Vortex Control. Volume 1 by : National Aeronautics and Space Administration (NASA)
Download or read book F/A-18 Forebody Vortex Control. Volume 1 written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-17 with total page 184 pages. Available in PDF, EPUB and Kindle. Book excerpt: A wind tunnel test was conducted on a six percent model of the F/A-18 at the NASA Ames 7 X 10-Foot Low Speed Wind Tunnel. The primary objective of the test was to evaluate several forebody vortex control configurations at high angles of attack in order to determine the most effective method of obtaining well behaved yawing moments, in preparation for the rotary balance test. Both mechanical and pneumatic systems were tested. Single and dual rotating nose tip strakes and a vertical nose strake were tested at different sizes and deflections. A series of jet blowing configurations were located at various fuselage stations, azimuth angles, and pointing angles ranging from straight aft to 60 deg canted inboard. Slot blowing was investigated for several slot lengths and fuselage stations. The effect of blowing rate was tested for both of these pneumatic systems. The most effective configurations were then further tested with a variation of both sideslip angle and Reynolds number over a range of angles of attack from 0 to 60 deg. It was found that a very robust system can be developed that provides yawing moments at angles of attack up to 60 deg that significantly exceeds that available from 30 deg of rudder deflection (F/A-18 maximum) at 0 deg angle of attack. Kramer, Brian R. and Suarez, Carlos J. and Malcolm, Gerald N. and Ayers, Bert F. Unspecified Center AIRCRAFT CONTROL; ANGLE OF ATTACK; BLOWING; F-18 AIRCRAFT; FOREBODIES; STRAKES; VORTICES; WIND TUNNEL TESTS; BOUNDARY LAYER CONTROL; LATERAL CONTROL; REYNOLDS NUMBER; YAWING MOMENTS...
Book Synopsis F/A-18 Forebody Vortex Control: Rotary-balance tests by :
Download or read book F/A-18 Forebody Vortex Control: Rotary-balance tests written by and published by . This book was released on 1994 with total page 228 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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Book Synopsis F/A-18 Forebody Vortex Control. Volume 2: Rotary-balance Tests by :
Download or read book F/A-18 Forebody Vortex Control. Volume 2: Rotary-balance Tests written by and published by . This book was released on 1994 with total page 228 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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Book Synopsis Aeronautical Enginnering: A Cumulative Index to a Continuing Bibliography (supplement 312) by :
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Book Synopsis Development of a Multicomponent Force and Moment Balance for Water Tunnel Applications, Volume 1 by :
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Book Synopsis Aerodynamic Control of NASP-type Vehicles Through Vortex Manipulation. Volume 1: Static Water Tunnel Tests by :
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Book Synopsis 32nd Aerospace Sciences Meeting & Exhibit: 94-0670 - 94-0709 by :
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