Experimental Study of Heat Transfer in a Critical Point of Sphere in Hypersonic Low-Density Flow,
Abstract
In an experimental study of heat transfer at the critical point of a sphere the possibility is confirmed of using underexpanded nozzles in hypersonic wind tunnels for radiation of the flow about the models over a wide range of Reynolds numbers. Experiments were carried out in a hypersonic shock tube with numbers M < 32.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 24, 1975
- Accession Number
- ADA007407
Entities
People
- V. N. Gusev
- Yu. V. Nikolskii
Organizations
- National Air and Space Intelligence Center