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The Design Of Supercritical Wings By The Use Of Three Dimensional Transonic Theory
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Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781725017184 Total Pages :34 pages Book Rating :4.0/5 (171 download)
Book Synopsis The Design of Supercritical Wings by the Use of Three-Dimensional Transonic Theory by : National Aeronautics and Space Administration (NASA)
Download or read book The Design of Supercritical Wings by the Use of Three-Dimensional Transonic Theory written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-08-13 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: A procedure was developed for the design of transonic wings by the iterative use of three dimensional, inviscid, transonic analysis methods. The procedure was based on simple principles of supersonic flow and provided the designer with a set of guidelines for the systematic alteration of wing profile shapes to achieve some desired pressure distribution. The method was generally applicable to wing design at conditions involving a large region of supercriterical flow. To illustrate the method, it was applied to the design of a wing for a supercritical maneuvering fighter that operates at high lift and transonic Mach number. The wing profiles were altered to produce a large region of supercritical flow which was terminated by a weak shock wave. The spanwise variation of drag of this wing and some principles for selecting the streamwise pressure distribution are also discussed. Mann, M. J. Langley Research Center NASA-TP-1400, L-12552 RTOP 505-11-13-03...
Book Synopsis NASA Technical Paper by : United States. National Aeronautics and Space Administration
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Book Synopsis Aerodynamic Design for Improved Maneuverability by Use of Three-dimensional Transonic Theory by : Michael J. Mann
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Book Synopsis Introduction to Transonic Aerodynamics by : Roelof Vos
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