Accession Number : AD0831414

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

Corporate Author : GENERAL DYNAMICS SAN DIEGO CA CONVAIR DIV

Personal Author(s) : Sergeant, R. J.

Report Date : 11 MAR 1959

Pagination or Media Count : 17

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.

Descriptors :   *EXHAUST FLAMES), (*VERNIER ROCKET ENGINES, (*AIRFRAMES, HEAT TRANSFER), CALORIMETERS, SURFACE TO SURFACE MISSILES, MODEL TESTS, SCALE, SPHERES, CYLINDRICAL BODIES, STAINLESS STEEL, TEST EQUIPMENT, TEMPERATURE, STABILIZATION, LIQUID PROPELLANT ROCKET ENGINES, CAPTIVE TESTS.

Subject Categories : Aircraft
      Thermodynamics
      Rocket Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE