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Effect Of Leading And Trailing Edge Flaps On Clipped Delta Wings With And Without Wing Camber At Supersonic Speeds
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Book Synopsis Effect of Leading- and Trailing-edge Flaps on Clipped Delta Wings with and Without Wing Camber at Supersonic Speeds by : Gloria Hernandez
Download or read book Effect of Leading- and Trailing-edge Flaps on Clipped Delta Wings with and Without Wing Camber at Supersonic Speeds written by Gloria Hernandez and published by . This book was released on 1994 with total page 112 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781723038570 Total Pages :106 pages Book Rating :4.0/5 (385 download)
Book Synopsis Effect of Leading- And Trailing-Edge Flaps on Clipped Delta Wings with and Without Wing Camber at Supersonic Speeds by : National Aeronautics and Space Administration (NASA)
Download or read book Effect of Leading- And Trailing-Edge Flaps on Clipped Delta Wings with and Without Wing Camber at Supersonic Speeds 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 106 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation of the aerodynamic characteristics of thin, moderately swept fighter wings has been conducted to evaluate the effect of camber and twist on the effectiveness of leading- and trailing-edge flaps at supersonic speeds in the Langley Unitary Plan Wind Tunnel. The study geometry consisted of a generic fuselage with camber typical of advanced fighter designs without inlets, canopy, or vertical tail. The model was tested with two wing configurations an uncambered (flat) wing and a cambered and twisted wing. Each wing had an identical clipped delta planform with an inboard leading edge swept back 65 deg and an outboard leading edge swept back 50 deg. The trailing edge was swept forward 25 deg. The leading-edge flaps were deflected 4 deg to 15 deg, and the trailing-edge flaps were deflected from -30 deg to 10 deg. Longitudinal force and moment data were obtained at Mach numbers of 1.60, 1.80, 2.00, and 2.16 for an angle-of-attack range 4 deg to 20 deg at a Reynolds number of 2.16 x 10(exp 6) per foot and for an angle-of-attack range 4 deg to 20 deg at a Reynolds number of 2.0 x 10(exp 6) per foot. Vapor screen, tuft, and oil flow visualization data are also included. Hernandez, Gloria and Wood, Richard M. and Covell, Peter F. Langley Research Center RESEARCH; INVESTIGATION; DESIGN; EXPLORATION...
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Book Synopsis Investigation of Leading-edge Flap Performance on Delta and Double-delta Wings at Supersonic Speeds by : Peter F. Covell
Download or read book Investigation of Leading-edge Flap Performance on Delta and Double-delta Wings at Supersonic Speeds written by Peter F. Covell and published by . This book was released on 1987 with total page 132 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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Book Synopsis Monthly Catalog of United States Government Publications by : United States. Superintendent of Documents
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