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Accession Number:
AD0641349
Title:
TABLES OF SUPERSONIC FLOWS ABOUT CONE CYLINDERS. PART II. COMPLETE FLOWS
Corporate Author:
ARMY BALLISTIC RESEARCH LAB ABERDEEN PROVING GROUND MD
Report Date:
1950-08-01
Abstract:
Cylindrical coordinates and velocity components were tabulated at points of a characteristic net for a family of steady, nonviscous, axisymmetric, irrotational supersonic flows about cone cylinders with semi cone angles of 5k degrees 1 or k or 10 and free stream Mach numbers 1.3, 1.5, 1.7, 2.0, 3. 0, 4.0, 5.0, and 7.0.
Supplementary Note:
See also PB-169-223.
Pages:
0254
Distribution Statement:
Approved for public release; distribution is unlimited.
File Size:
11.24MB
