Accession Number:

AD0681059

Title:

CALCULATION OF A MIXED SUB- AND SUPERSONIC GAS FLOW IN A PLANE PRESSURE NOZZLE,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1968-01-17

Pagination or Media Count:

11.0

Abstract:

A plane potential subsonic and supersonic flow of gas is analyzed without taking into account the viscosity and heat conduction. A particular solution, corresponding to the motion of a gas in a nozzle with a curvilinear sonic line, was obtained for the system of mixed elliptic-hyperbolic equations of motion in the potential plane. The accuracy of the simplifications used in the analysis was verified by exact calculations and experiments. Author

Subject Categories:

  • Aerodynamics
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE