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An Approximate Method For Calculating Three Dimensional Inviscid Hypersonic Flow Fields
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Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722063351 Total Pages :28 pages Book Rating :4.0/5 (633 download)
Book Synopsis An Approximate Method for Calculating Three-Dimensional Inviscid Hypersonic Flow Fields by : National Aeronautics and Space Administration (NASA)
Download or read book An Approximate Method for Calculating Three-Dimensional Inviscid Hypersonic Flow Fields written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-06-30 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: An approximate solution technique was developed for 3-D inviscid, hypersonic flows. The method employs Maslen's explicit pressure equation in addition to the assumption of approximate stream surfaces in the shock layer. This approximation represents a simplification to Maslen's asymmetric method. The present method presents a tractable procedure for computing the inviscid flow over 3-D surfaces at angle of attack. The solution procedure involves iteratively changing the shock shape in the subsonic-transonic region until the correct body shape is obtained. Beyond this region, the shock surface is determined using a marching procedure. Results are presented for a spherically blunted cone, paraboloid, and elliptic cone at angle of attack. The calculated surface pressures are compared with experimental data and finite difference solutions of the Euler equations. Shock shapes and profiles of pressure are also examined. Comparisons indicate the method adequately predicts shock layer properties on blunt bodies in hypersonic flow. The speed of the calculations makes the procedure attractive for engineering design applications. Riley, Christopher J. and Dejarnette, Fred R. Langley Research Center RTOP 506-40-91-01...
Book Synopsis An Approximate Method for Calculating Three-Dimensional Inviscid Hypersonic Flow Fields by : National Aeronautics and Space Administration NASA
Download or read book An Approximate Method for Calculating Three-Dimensional Inviscid Hypersonic Flow Fields written by National Aeronautics and Space Administration NASA and published by . This book was released on 2018-10-23 with total page 27 pages. Available in PDF, EPUB and Kindle. Book excerpt: An approximate solution technique was developed for 3-D inviscid, hypersonic flows. The method employs Maslen's explicit pressure equation in addition to the assumption of approximate stream surfaces in the shock layer. This approximation represents a simplification to Maslen's asymmetric method. The present method presents a tractable procedure for computing the inviscid flow over 3-D surfaces at angle of attack. The solution procedure involves iteratively changing the shock shape in the subsonic-transonic region until the correct body shape is obtained. Beyond this region, the shock surface is determined using a marching procedure. Results are presented for a spherically blunted cone, paraboloid, and elliptic cone at angle of attack. The calculated surface pressures are compared with experimental data and finite difference solutions of the Euler equations. Shock shapes and profiles of pressure are also examined. Comparisons indicate the method adequately predicts shock layer properties on blunt bodies in hypersonic flow. The speed of the calculations makes the procedure attractive for engineering design applications. Riley, Christopher J. and Dejarnette, Fred R. Langley Research Center RTOP 506-40-91-01...
Book Synopsis An Approximate Method for Calculating Three-dimensional Inviscid Hypersonic Flow Fields by : Christopher Joseph Riley
Download or read book An Approximate Method for Calculating Three-dimensional Inviscid Hypersonic Flow Fields written by Christopher Joseph Riley and published by . This book was released on 1990 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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