Steady and Unsteady Transonic Pressure Measurements on a Clipped Delta Wing for Pitching and Control-surface Oscillations

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Total Pages : 124 pages
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Book Synopsis Steady and Unsteady Transonic Pressure Measurements on a Clipped Delta Wing for Pitching and Control-surface Oscillations by :

Download or read book Steady and Unsteady Transonic Pressure Measurements on a Clipped Delta Wing for Pitching and Control-surface Oscillations written by and published by . This book was released on 1986 with total page 124 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Steady and Unsteady Transonic Pressure Measurements on a Clipped Delta Wing for Pitching and Control-surface Oscillations

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ISBN 13 :
Total Pages : 115 pages
Book Rating : 4.:/5 (14 download)

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Book Synopsis Steady and Unsteady Transonic Pressure Measurements on a Clipped Delta Wing for Pitching and Control-surface Oscillations by : Robert W. Hess

Download or read book Steady and Unsteady Transonic Pressure Measurements on a Clipped Delta Wing for Pitching and Control-surface Oscillations written by Robert W. Hess and published by . This book was released on 1986 with total page 115 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Computational Test Cases for a Clipped Delta Wing with Pitching and Trailing-Edge Control Surface Oscillations

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ISBN 13 :
Total Pages : 96 pages
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Book Synopsis Computational Test Cases for a Clipped Delta Wing with Pitching and Trailing-Edge Control Surface Oscillations by : Robert M. Bennett

Download or read book Computational Test Cases for a Clipped Delta Wing with Pitching and Trailing-Edge Control Surface Oscillations written by Robert M. Bennett and published by . This book was released on 1999 with total page 96 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Static and Unsteady Pressure Measurements on a 50 Degree Clipped Delta Wing at M

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ISBN 13 :
Total Pages : 16 pages
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Book Synopsis Static and Unsteady Pressure Measurements on a 50 Degree Clipped Delta Wing at M by :

Download or read book Static and Unsteady Pressure Measurements on a 50 Degree Clipped Delta Wing at M written by and published by . This book was released on 1982 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Scientific and Technical Publications

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ISBN 13 :
Total Pages : 178 pages
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Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 702 pages
Book Rating : 4.:/5 (3 download)

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Monthly Catalog of United States Government Publications

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ISBN 13 :
Total Pages : 1102 pages
Book Rating : 4.3/5 (243 download)

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Download or read book Monthly Catalog of United States Government Publications written by and published by . This book was released on 2004 with total page 1102 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Computational Test Cases for a Clipped Delta Wing with Pitching and Trailing-Edge Control Surface Oscillations

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Publisher : Independently Published
ISBN 13 : 9781723946066
Total Pages : 92 pages
Book Rating : 4.9/5 (46 download)

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Book Synopsis Computational Test Cases for a Clipped Delta Wing with Pitching and Trailing-Edge Control Surface Oscillations by : National Aeronautics and Space Adm Nasa

Download or read book Computational Test Cases for a Clipped Delta Wing with Pitching and Trailing-Edge Control Surface Oscillations written by National Aeronautics and Space Adm Nasa and published by Independently Published. This book was released on 2018-09-23 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt: Computational test cases have been selected from the data set for a clipped delta wing with a six-percent-thick circular-arc airfoil section that was tested in the NASA Langley Transonic Dynamics Tunnel. The test cases include parametric variation of static angle of attack, pitching oscillation frequency, trailing-edge control surface oscillation frequency, and Mach numbers from subsonic to low supersonic values. Tables and plots of the measured pressures are presented for each case. This report provides an early release of test cases that have been proposed for a document that supplements the cases presented in AGARD Report 702.Bennett, Robert M. and Walker, Charlotte E.Langley Research CenterCOMPUTATIONAL FLUID DYNAMICS; DELTA WINGS; AIRFOIL PROFILES; CONTROL SURFACES; PITCH (INCLINATION); WIND TUNNEL TESTS; UNSTEADY AERODYNAMICS; TRANSONIC FLOW; COMPUTERIZED SIMULATION; ANGLE OF ATTACK; TRAILING EDGES; MACH NUMBER; WIND TUNNEL MODELS; ATTITUDE CONTROL; OSCILLATIONS

Test Cases for a Clipped Delta Wing with Pitching and Trailing-Edge Control Surface Oscillations

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ISBN 13 :
Total Pages : 18 pages
Book Rating : 4.:/5 (228 download)

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Book Synopsis Test Cases for a Clipped Delta Wing with Pitching and Trailing-Edge Control Surface Oscillations by : Robet M. Bennett

Download or read book Test Cases for a Clipped Delta Wing with Pitching and Trailing-Edge Control Surface Oscillations written by Robet M. Bennett and published by . This book was released on 2000 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt: Steady and unsteady measured pressures for a Clipped Delta Wing (CDW) undergoing pitching oscillations and trailing-edge control surface oscillations have been presented in Ref I and 2. From the several hundred compiled data points, 22 static cases, 12 pitching-oscillation cases, and 12 control-surface-oscillation cases have been proposed for Computational Test Cases to illustrate the trends with Mach number, reduced frequency, and angle of attack. The planform for this wing was derived by simplifying the planform of a proposed design for a supersonic transport which is described (Ref 3) as the Boeing 2707-300. The strake was deleted. the resulting planform was approximated by a trapezoid with an unswept trailing edge, and the twist and camber were removed. In order to facilitate pressure instrumentation, the thickness was increased to 6 percent from the typical 2.1 to 3 percent for the supersonic transport. The airfoil is thus a symmetrical circular arc Section with tie 0.06 of similar planform but with a thinner airfoil of tic 0.03 was used in the flutter investigations of Ref 4 and 5, and the buffet and stall flutter investigation of Ref 6. Flutter results are also reported both for the 3 per event thick simplified wing and for a more complex SST model in Ref 7.

NASA Technical Memorandum

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ISBN 13 :
Total Pages : 496 pages
Book Rating : 4.:/5 (319 download)

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NASA Scientific and Technical Publications

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ISBN 13 :
Total Pages : 180 pages
Book Rating : 4.3/5 ( download)

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Download or read book NASA Scientific and Technical Publications written by and published by . This book was released on 1987 with total page 180 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Conference Publication

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ISBN 13 :
Total Pages : 458 pages
Book Rating : 4.F/5 ( download)

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Download or read book NASA Conference Publication written by and published by . This book was released on 1999 with total page 458 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Recent Transonic Unsteady Pressure Measurements at the NASA Langley Research Center

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ISBN 13 :
Total Pages : 24 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Recent Transonic Unsteady Pressure Measurements at the NASA Langley Research Center by :

Download or read book Recent Transonic Unsteady Pressure Measurements at the NASA Langley Research Center written by and published by . This book was released on 1985 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Integral-equation Methods in Steady and Unsteady Subsonic, Transonic and Supersonic Aerodynamics for Interdisciplinary Design

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ISBN 13 :
Total Pages : 20 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Integral-equation Methods in Steady and Unsteady Subsonic, Transonic and Supersonic Aerodynamics for Interdisciplinary Design by :

Download or read book Integral-equation Methods in Steady and Unsteady Subsonic, Transonic and Supersonic Aerodynamics for Interdisciplinary Design written by and published by . This book was released on 1990 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:

CEAS/AIAA/ICASE/NASA Langley International Forum on Aeroelasticity and Structural Dynamics 1999

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ISBN 13 :
Total Pages : 460 pages
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Book Synopsis CEAS/AIAA/ICASE/NASA Langley International Forum on Aeroelasticity and Structural Dynamics 1999 by :

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Scientific and Technical Information Output of the Langley Research Center for Calendar Year 1986

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ISBN 13 :
Total Pages : 270 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Scientific and Technical Information Output of the Langley Research Center for Calendar Year 1986 by : Langley Research Center. Research Information and Applications Division

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Close-range Photogrammetric Measurement of Static Deflections for an Aeroelastic Supercritical Wing

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ISBN 13 :
Total Pages : 100 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Close-range Photogrammetric Measurement of Static Deflections for an Aeroelastic Supercritical Wing by : Thomas A. Byrdsong

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