Accession Number:

AD0091959

Title:

PERFORMANCE OF SUPERSONIC RAMP-TYPE SIDE INLET WITH COMBINATIONS OF FUSELAGE AND INLET THROAT BOUNDARY-LAYER REMOVAL

Descriptive Note:

Research memo.

Corporate Author:

NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON DC

Personal Author(s):

Report Date:

1956-04-25

Pagination or Media Count:

25.0

Abstract:

Subject Categories:

  • Aircraft
  • Pumps, Filters, Pipes, Tubing, Fittings and Valves

Distribution Statement:

APPROVED FOR PUBLIC RELEASE