Accession Number : ADA952911

Title :   Preliminary Study of a Supersonic Induction Type Wind Tunnel for Cornell Aeronautical Laboratory.

Descriptive Note : Technical memo.,

Corporate Author : CORNELL AERONAUTICAL LAB INC BUFFALO N Y

Personal Author(s) : Moore,J. L. ; Finamore,O. B. ; Wilder,J. G.

Report Date : 22 SEP 1947

Pagination or Media Count : 38

Descriptors :   *Supersonic wind tunnels, Induction systems, High pressure, Volume, Thermodynamics, Air flow, Mixing

Subject Categories : Test Facilities, Equipment and Methods

Distribution Statement : APPROVED FOR PUBLIC RELEASE