Accession Number : AD0693287

Title :   SUPERSONIC GAS FLOW PAST BLUNT BODIES. THEORETICAL AND EXPERIMENTAL STUDIES.

Descriptive Note : 2ND ED.,

Corporate Author : ARMY FOREIGN SCIENCE AND TECHNOLOGY CENTER WASHINGTON D C

Personal Author(s) : Belotserkovskii,O. M. ; Bulekbaev,A. ; Golomazov,M. M. ; Grudnitskii,V. G. ; Bushim,V. K.

Report Date : 1969

Pagination or Media Count : 377

Abstract : Over a number of years formulation of numerical algorithms for calculating flow past blunt bodies with detached shock wave has been underway in the Computation Center of the USSR Academy of Sciences and the Leningrad Engineering Physics Institute. This review dwells on several features in the use of the method of integral relations for this problem and describes the construction of numerical algorithms, and demonstrates their use for various cases of streamline flow. (Author)

Descriptors :   (*NOSE CONES, ATMOSPHERE ENTRY), (*REENTRY VEHICLES, SUPERSONIC CHARACTERISTICS), ALGORITHMS, JET MIXING FLOW, FROZEN EQUILIBRIUM FLOW, BODIES OF REVOLUTION, EQUATIONS OF MOTION, THREE DIMENSIONAL FLOW, ENTROPY, WIND TUNNEL MODELS, USSR

Subject Categories : Guided Missile Dynam, Config & Cntrl Surfaces
      Guided Missile Reentry Vehicles

Distribution Statement : APPROVED FOR PUBLIC RELEASE