Special Course on Aerothermodynamics of Hypersonic Vehicles
Abstract
Following the review of basic principles including real gas effects, a series of lectures were presented on experimental and computational methods specific to hypersonic flows. Stress was placed on measurement techniques developed primarily for flows with heat transfer, chemical reactions, strong shocks, compressible boundary layers, etc. Both surface measurements and flow field measurements including species concentration techniques, were discussed. The same spirit governed the lecture on computational methods: stress was placed on the new problems in CFD posed by high speeds and chemical reactions. The course finished with state-of-the-art reviews on three critical flow problems: transition to turbulence, interactions between shocks and boundary layers, and shock/shock impingement. Keywords: Lectures; Hypersonic flow; Computation; Shock waves; Chemical reactions; Aerothermodynamics; Measurement.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 01, 1989
- Accession Number
- ADA214027
Entities
Organizations
- AGARD