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

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

Title: The Calculation of Nonlinear Supersonice Conical Flows by the Method of Integral Relations
Date: 1964
Index Abstract: Not Available
Photo Quality: Not Needed
Report Number: FDL TDR 64-7
Creator: Brook, John W.
Corporate Author: Grumman Aircraft Engineering Corporation
Extent: 106
Identifier: AD0605284
Access Rights: OTS
Distribution Classification: 1
Contract: AF 33(657)-7313
DoD Project: 8219
DoD Task: 821902
DTIC Record Exists: No
Distribution Change Authority Correspondence: None
Abstract: 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.
Report Availability: Full text available
Date Issued: 1964-07
Laboratory: AF Flight Dynamics Laboratory
Provenance: AFRL/VACA
Type: report
Format: 1 online resource