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Accession Number:
AD0753696
Title:
The Calculation of Three-Dimensional Supersonic Flows around Spherically-Capped Smooth Bodies and Wings. Volume II. Manual for Computer Programs.
Corporate Author:
NORTHROP CORP HAWTHORNE CALIF AIRCRAFT DIV
Report Date:
1972-09-01
Abstract:
I Powers,Sidney A. NOR-72-87-Vol-2F33615-72-C-1429AF-1366AFFDLTR-72-91-Vol-2See also Volume 1, AD-753 695.airframes, supersonic characteristics, computer programs, aerodynamics, numerical analysis, conical bodies, delta wings, instruction manuals, blunt bodies, hypersonic characteristics, angle of attack, three dimensional flow, subroutinescomputer aided analysis, smooth bodies, inviscid flowThe report describes the theories, the numerical methods and the computer programs developed for determining the inviscid three-dimensional flow about smooth shapes at supersonic speeds. Volume II is a users manual for the computer programs and provides the detailed information needed to set up and use the programs. These programs can determine the supersonic flow past smooth blunted bodies for any angle of attack for which the initial value surface remains on the blunted nose. The lowest usable Mach number is on the order of 2.0, with lower values attainable by careful attention to the initial value surface solution. There is no computational upper limit on the Mach number. Author
Descriptive Note:
Final rept. 1 Dec 71-3 Jul 72,
Supplementary Note:
See also Volume 1, AD-753 695.
Pages:
0205
Contract Number:
F33615-72-C-1429
File Size:
0.00MB
