Accession Number : ADA952969

Title :   Two-Dimensional Supersonic Wind Tunnel Investigations of Flow in a Duct with Flutuating Exit Pressure. Part 1. Experimental Technique.

Descriptive Note : Technical memo.,

Corporate Author : CORNELL AERONAUTICAL LAB INC BUFFALO N Y

Personal Author(s) : Kamrass,M.

Report Date : 30 JUN 1947

Pagination or Media Count : 15

Descriptors :   *Supersonic flow, Ducts, Gas flow, Fluid mechanics, Wind tunnel tests, Two dimensional

Subject Categories : Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE