Accession Number:

AD0094239

Title:

DYNAMICS OF A SUPERSONIC INLET WITH ADJUSTABLE BYPASS IN COMBINATION WITH A J34 TURBOJET ENGINE

Descriptive Note:

Research memo.

Corporate Author:

NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON DC

Personal Author(s):

Report Date:

1956-03-23

Pagination or Media Count:

31.0

Abstract:

Subject Categories:

  • Fluid Mechanics
  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE