The Calculation of Nonlinear Supersonice Conical Flows by the Method of Integral Relations

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Report Number: FDL TDR 64-7
Author(s): Brook, John W.
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-07
Pages: 106
Contract: AF 33(657)-7313
DoD Project: 8219
DoD Task: 821902
Identifier: AD0605284

The supersonic flow over cones of arbitrary shape was investigated by using the method of integral relations. The equations are derived for one strip using a body-oriented coordinate system. Various choices for basic equations are discussed. The solution of the boundary value problem for a number of fundamentally different cases is discussed in detail and various suggestions concerning improvements of the method and other related methods are made. Due to severe computational difficulties, however, no numerical results are presented.

Provenance: AFRL/VACA

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