Accession Number : AD0754606

Title :   Determination of Optimum Parameters of the Means Used to Protect the Compartments of an Aircraft from Aerodynamic Heat at High Speeds and during a Prolonged Flight,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Yasinskii,F. G. ; Kobylyanskii,A. A.

Report Date : 05 JAN 1973

Pagination or Media Count : 19

Abstract : Optimum parameters of the means used to protect the aircraft compartments from aerodynamic heat are determined. The thermal conductivity coefficient is expressed in the form of a linear temperature function when studying the external and internal heat insulators. Coupling equations are used in computations using electronic digital computer. (Author)

Descriptors :   (*THERMAL INSULATION, THERMAL CONDUCTIVITY), (*SUPERSONIC AIRCRAFT, *AERODYNAMIC HEATING), AIRFRAMES, COOLING, HEAT TRANSFER, THERMAL STRESSES, MATHEMATICAL MODELS, OPTIMIZATION, USSR

Subject Categories : Aircraft
      Thermodynamics

Distribution Statement : APPROVED FOR PUBLIC RELEASE