LOW DENSITY HIGH TEMPERATURE GAS DYNAMICS.
Abstract
A summary is given of low density hypersonic flow research. Progress is reported on wind tunnel instrumentation based upon a technique which takes advantage of a periodic modulation of the flow to improve the signalto-noise ratio of the instruments, which include hot wire probes and force measuring balances. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 01, 1966
- Accession Number
- AD0629779
Entities
People
- J. J. Smolderen
Organizations
- von Kármán Institute for Fluid Dynamics