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Accession Number:
AD0494220
Title:
SOME COMMENTS ON THE FORM OF THE DRAG COEFFICIENT AT SUPERSONIC VELOCITY
Corporate Author:
ARMY BALLISTIC RESEARCH LAB ABERDEEN PROVING GROUND MD
Report Date:
1942-04-20
Abstract:
A form of representation of the drag curve at supersonic velocity is suggested. Only two unknown constants are required for each shell, hence firings at two velocities fix the function. For the case of a conical head and square base, the problem can be reduced to one constant. Good experimental confirmation is found.
Supplementary Note:
DOI: 10.21236/AD0494220
Pages:
0044
Distribution Statement:
Approved for public release; distribution is unlimited. Document partially illegible.
File Size:
3.47MB
