Accession Number : AD0696049

Title :   GAS DYNAMICS OF SOLID-PROPELLANT ROCKET ENGINES,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Shishkov,A. A.

Report Date : 23 APR 1969

Pagination or Media Count : 188

Abstract : In this book an attempt is made to give an account of engineering methods of gas-dynamic calculation of the solid-propellant rocket engine from the single view-point based on principles of applied gas dynamics. (Author)

Descriptors :   (*SOLID PROPELLANT ROCKET ENGINES, NOZZLE GAS FLOW), EQUATIONS OF MOTION, BURNING RATE, EROSIVE BURNING, COMBUSTION, HEAT TRANSFER, STAGNATION POINT, INCOMPRESSIBLE FLOW, TURBULENCE, INTERIOR BALLISTICS, ROCKET NOZZLES, THRUST, COMBUSTION PRODUCTS, FLOW SEPARATION, JET MIXING FLOW, ONE DIMENSIONAL FLOW, TWO DIMENSIONAL FLOW, USSR

Subject Categories : Fluid Mechanics
      Solid Propellant Rocket Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE