Download or read book Measurements of Unsteady Pressure and Structural Response for an Elastic Supercritical Wing written by Clinton V. Eckstrom and published by . This book was released on 1994 with total page 144 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Unsteady Pressure and Structural Response Measurements of an Elastic Supercritical Wing written by and published by . This book was released on 1988 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Measurements of Unsteady Pressure and Structural Response for an Elastic Supercritical Wing written by National Aeronautics and Space Adm Nasa and published by . This book was released on 2018-11-17 with total page 142 pages. Available in PDF, EPUB and Kindle. Book excerpt: Results are presented which define unsteady flow conditions associated with the high-dynamic structural response of a high-aspect-ratio, elastic, supercritical wing at transonic speeds. The wing was tested in the Langley Transonic Dynamics Tunnel with a heavy gas test medium. The supercritical wing, designed for a cruise lift coefficient of 0.53 at a Mach number of 0.80, experienced the high-dynamic structural response from Mach 0.90 to 0.94 with the maximum response occurring at about Mach 0.92. At the maximum response conditions of the wing, the forcing function appears to be the oscillatory chordwise movement of strong shocks located on the upper and lower surfaces of the wing in conjunction with the flow separation on the lower surface of the wing in the trailing-edge cove region. Eckstrom, Clinton V. and Seidel, David A. and Sandford, Maynard C. Langley Research Center AEROELASTICITY; DYNAMIC RESPONSE; PRESSURE DISTRIBUTION; SUPERCRITICAL WINGS; TRANSONIC SPEED; UNSTEADY FLOW; WIND TUNNEL TESTS; AERODYNAMIC COEFFICIENTS; BOUNDARY LAYER SEPARATION; SEPARATED FLOW; SLENDER WINGS; TRAILING EDGES; TRANSONIC WIND TUNNELS...
Download or read book Unsteady pressure and Dynamic deflection Measurements on an Aeroelastic Supercritical Wing written by David A. Seidel and published by . This book was released on 1991 with total page 330 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 464 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Download or read book Monthly Catalog of United States Government Publications written by and published by . This book was released on with total page 1224 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Monthly Catalogue United States Public Documents written by and published by . This book was released on 1995-11 with total page 944 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Memorandum written by and published by . This book was released on 1992 with total page 332 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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Download or read book Close range Photogrammetric Measurement of Static Deflections for an Aeroelastic Supercritical Wing written by Thomas A. Byrdsong and published by . This book was released on 1990 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book A Collection of Technical Papers written by and published by . This book was released on 1988 with total page 632 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Steady Pressure Measurements on an Aeroelastic Research Wing ARW 2 written by Maynard C. Sandford and published by . This book was released on 1994 with total page 582 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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Download or read book Geometric and Structural Properties of a Rectangular Supercritical Wing Oscillated in Pitch for Measurement of Unsteady Transonic Pressure Distributions written by and published by . This book was released on 1983 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Feasibility of Using a Knowledge based System Concept for In flight Primary Flight Display Research written by David A. Seidel and published by . This book was released on 1991 with total page 588 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book 30th AIAA Fluid Dynamics Conference written by and published by . This book was released on 1999 with total page 620 pages. Available in PDF, EPUB and Kindle. Book excerpt:
