Accession Number : AD0270763

Title :   THE EFFECT OF VISCOSITY AND HEAT CONDUCTION ON THE FLOW OF A GAS BEHIND A SEVERELY CURVED SHOCK WAVE

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : LYUBIMOV,G.A.

Report Date : 25 JAN 1962

Pagination or Media Count : 1

Abstract : Formulas are derived for the relation of stagnation temperatures and pressures behind and in front of a shock wave of any shape, taking into account the viscosity and thermal conductivity of a gas. (Author)

Descriptors :   *SHOCK WAVES, GAS FLOW, HEAT TRANSFER, MATHEMATICAL ANALYSIS, MATHEMATICAL PREDICTION, PRESSURE, TEMPERATURE, THEORY, TRANSLATIONS, VISCOSITY

Distribution Statement : APPROVED FOR PUBLIC RELEASE