Accession Number:

AD0258223

Title:

Notes on Analytical Techniques in Aerodynamic Heating Problems

Descriptive Note:

Corporate Author:

NAVAL ORDNANCE TEST STATION CHINA LAKE CA

Report Date:

1961-04-28

Pagination or Media Count:

44.0

Abstract:

TEMPERATURE CHANGES DURING HEATING OF AN HPAG 5.0-INCH MOTOR CORRELATION OF EXPERIMENTAL DATA WITH ANALOG COMPUTATIONS, by C. H. Johnson Temperature data on a 5.0-inch HPAG rocket motor served to guide the set up of an analog computer model. The study was prompted by observations that temperatures in heated Sidewinder 1C motors differed appreciably depending on whether the test point was at the top, side, or bottom of the motor. DETERMINATION OF WALL TEMPERATURE-TIME FUNCTIONS USING AN ANALOG COMPUTER, by William H. Smith The use of an analog computer to obtain solutions of the outside surface temperature of aerodynamically heated bodies resulted in a large saving over hand solutions. WHEN IS A SKIN THERMALLY THIN, by Jerome R. Katz A method for determining skin thickness is discussed for 1, 5, and 10 variations in temperature throughout the material.

Subject Categories:

  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE