Computation of transonic potential flow about three-dimensional inlets, ducts, and bodies
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Computation of transonic potential flow about three-dimensional inlets, ducts, and bodies

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Published by National Aeronautics and Space Administration, Scientific and Technical Information Branch, For sale by the National Technical Information Service] in Washington, D.C, [Springfield, Va .
Written in English

Subjects:

  • Aerodynamics -- Data processing,
  • Aerodynamics -- Mathematical models

Book details:

Edition Notes

StatementTheodore A. Reyhner ; prepared under Cooperative Agreement with NASA Langley Research Center and Boeing, Commercial Airplane Company
SeriesNASA contractor report -- 3514
ContributionsUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Langley Research Center, Boeing Commercial Airplane Company
The Physical Object
Paginationx, 83 p. :
Number of Pages83
ID Numbers
Open LibraryOL14930873M

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Computation of transonic potential flow about three-dimensional inlets, ducts, and bodies. Washington, D.C.: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. An analysis was developed and a computer code, P Version A, written for the prediction of transonic potential flow about three dimensional objects including inlet, duct, and body geometries. Finite differences and line relaxation are used to solve the complete potential flow equation. An analysis was developed and a computer code, P Version A, written for the prediction of transonic potential flow about three dimensional objects including inlet, duct, and body geometries. Finite differences and line relaxation are used to solve the complete potential flow : T. A. Reyhner. Computation of transonic potential flow about three-dimensional inlets, ducts, and bodies / By Theodore A. Reyhner, Boeing Commercial Airplane Company., Langley Research Center. and United States. National Aeronautics and Space Administration.

  Computation of transonic potential flow past wing-body configurations Acta Mechanica, Vol. 81, No. Euler correction method for two- and three-dimensional transonic flowsCited by: Calculation of Transonic Potential Flow Past ThreeDimensional Configurations D. A. Caughey 1. INTRODUCTION. In recent years, substantial progress has been made in the development of efficient algorithms for solving discrete approximations to the potential equation for transonic (i.e., mixed subsonic and supersonic) flow past rather general geometrical : D.A. Caughey. AN establishment method is used for the numerical investigation of inviscid, thermally non-conducting gas flow in nozzles involving transonic velociti Author: Ivanov, O.A. Ryl'ko. This simple method can be applied to generate grids for arbitrary fuselage fitted with any swept wing with dihedral. Three dimensional transonic analysis code TWING, with approximate factorization (AF2) scheme has been suitably used as a flow solver. As an example, RAE-WING-A with body-B2 configuration has been by: 5.

Transonic Potential Flow Computation about Three-Dimensional Inlets, Ducts, and Bodies. T. A. Reyhner ; 17 May | AIAA Journal, Vol. 19, No. 9. Investigation of Transonic Flow in a Cascade Using the Finite Element by:   Computation of three dimensional transonic flows using two stream functions. M. HAFEZ; EXPERIENCES IN USING THE CYBER AND CYBER FOR THREE-DIMENSIONAL TRANSONIC FLOW CALCULATIONS. Transonic potential flow computation about three-dimensional inlets,ducts and bodies. T. REYHNER; 13th Fluid and PlasmaDynamics Conference . D.A. Caughey, Calculation of Transonic Potential Flow Past Three-Dimensional Configurations, Transonic, Shock, and Multidimensional Flows, /B Cited by: Transonic Potential Flow around Axisymmetric Inlets and Bodies at Angle of Attack. T. A. Reyhner ; T. A. Reyhner. Boeing Commercial Airplane Company, Seattle, Wash. Search for more papers by Cited by: