Accession Number:

AD0657775

Title:

RESEARCH ON ADVANCED GASDYNAMICS TEST FACILITIES.

Descriptive Note:

Final rept.,

Corporate Author:

CORNELL AERONAUTICAL LAB INC BUFFALO N Y

Report Date:

1967-04-01

Pagination or Media Count:

129.0

Abstract:

The report describes studies carried out on methods of improving the performance of conventional shock tubes and shock tunnels, on problems peculiar to high enthalpy test facilities, and on the application of lasers to aerodynamic facilities. A number of the studies carried out have previously been described in detail in separate reports or papers and these are summarized those previously unreported, in particular the laser application studies and recent isentropic compression tube studies, are described in detail. Author

Subject Categories:

  • Aerodynamics
  • Lasers and Masers
  • Test Facilities, Equipment and Methods
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE