Accession Number:

AD0831414

Title:

FURTHER INVESTIGATION OF HEATING RATES TO SPHERICAL AND CYLINDRICAL BODIES IN A 1/10 SCALE ATLAS VERNIER ROCKET ENGINE EXHAUST,

Personal Author(s):

Corporate Author:

GENERAL DYNAMICS SAN DIEGO CA CONVAIR DIV

Report Date:

1959-03-11

Abstract:

Object To determine the stagnation point heating rate to spherical and cylindrical bodies of the same diameter at various locations in the highly expanded exhaust jet of a scale vernier rocket.

Pages:

0017

Subject Categories:

Communities Of Interest:

File Size:

0.00MB

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