[PDF] e-Book A Method Of Characteristics For Steady Three Dimensional Supersonic Flow With Application To Inclined Bodies Of Revolution Full Read

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Language: en
Pages: 68

A Method of Characteristics for Steady Three-dimensional Supersonic Flow with Application to Inclined Bodies of Revolution

Authors: John V. Rakich

Categories: Aerodynamics, Supersonic

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Characteristics method for determining three dimensional supersonic flow around inclined body of revolution.

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The Calculation of Three-dimensional Supersonic Flows Around Spherically-capped Smooth Bodies and Wings: Theory and applications

Authors: Chong-Wei Chu

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NASA Technical Note

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Type: BOOK - Published: 1972 - Publisher:

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Language: en
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Prediction of Centerline Shock-layer Thickness and Pressure Distribution on Delta Wing-body Configurations

Authors: George E. Kaattari

Categories: Angle of attack (Aerodynamics)

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Language: en
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Calculation of the Boundary-layer Flow in the Windward Symmetry Plane of a Spherically Blunted Axisymmetric Body at Angle of Attack, Including Streamline-swallowing Effects

Authors: Arloe W. Mayne (Jr.)

Categories: Aerodynamics, Hypersonic

Type: BOOK - Published: 1973 - Publisher:

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Three-dimensional compressible boundary-layer equations are particularized to the windward symmetry plane of a spherically blunted axisymmetric body at incidenc