Accession Number:

AD0626940

Title:

RESEARCH ON ADVANCED GASDYNAMIC FACILITIES.

Descriptive Note:

Summary rept.,

Corporate Author:

CORNELL AERONAUTICAL LAB INC BUFFALO N Y

Personal Author(s):

• Hall ,J. Gordon
• Lordi ,J. A.
• Fetz ,B. H.
• Stoddard ,F.
• Bartz,J.

Report Date:

1965-10-01

Pagination or Media Count:

70.0

Abstract:

The report describes studies on methods of increasing the performance of conventional shock tubes and tunnels, and on problems peculiar to high enthalpy test facilities. A number of the studies carried out have previously been described in detail in separate reports or papers and are only summarized herein those previously unreported are described in detail. Author

Descriptors:

• *GAS FLOW
• *SHOCK TUBES
• TEST FACILITIES
• PERFORMANCE(ENGINEERING)
• PERFORMANCE(ENGINEERING)
• NOZZLE THROATS
• ENTHALPY
• NONEQUILIBRIUM FLOW

Subject Categories:

• Test Facilities, Equipment and Methods
• Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE