Accession Number:

AD0092794

Title:

TRANSONIC WIND-TUNNEL INVESTIGATION OF THE EFFECTS OF A HEATED PROPULSIVE JET ON THE PRESSURE DISTRIBUTION ALONG A FUSELAGE OVERHANG

Descriptive Note:

Research memo.

Corporate Author:

NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA

Personal Author(s):

Report Date:

1956-04-04

Pagination or Media Count:

47.0

Abstract:

Subject Categories:

  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE