Accession Number:

AD0270763

Title:

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

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1962-01-25

Pagination or Media Count:

1.0

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

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE