Accession Number:

ADA007458

Title:

Flows with Lambda-Shaped Shocks at the Entrance into Plane Supersonic Air Inlet,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1975-02-04

Pagination or Media Count:

27.0

Abstract:

Subject Categories:

  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE