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) : CORNETTE, ELDEN S ; WARD, DONALD H


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/092794.pdf


Report Date : 04 Apr 1956


Pagination or Media Count : 47


Descriptors :   *JET MIXING FLOW , FUSELAGES , JET PROPULSION , TRANSONIC CHARACTERISTICS , THERMODYNAMICS , PRESSURE DISTRIBUTION


Subject Categories : Fluid Mechanics


Distribution Statement : APPROVED FOR PUBLIC RELEASE