Fast-response, electronically-scanned multi-port pressure system for low-pressure hypersonic wind tunnel applications
- 20 June 1994
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Joint computational/experimental aerodynamics research on hypersonicvehicle. II - Computational resultsAIAA Journal, 1992
- DIGITAL COMPUTER ORIENTED METHODS FOR DETERMINING THE RESPONSE OF PRESSURE MEASUREMENT SYSTEMS TO STEP AND RAMP FORCING FUNCTIONSPublished by Defense Technical Information Center (DTIC) ,1967