Experimental Hypersonic Shock/Boundary-LayerInteraction Studies on a Flat Plate at Elevated Surface Temperature
Abstract
1. Evaluation of an existing experimental database recently collected on a temperature variable flat plate model in HEG with compression corner. The evaluation will reveal the capabilities and limitations of an experimental investigation of SBLI using the setup introduced in section 2. 2. Based on the first objective the wind tunnel model setup and the measurementtechniques will be adapted to address identified deficiencies. A series of tests at test conditions defined in close cooperation with the colleagues at University of Maryland will be conducted providing valuable experimental data for code validation. 3. Investigation of the effect of modified thermo-chemistry on SBLI gaining in importance in hypervelocity flows.
Document Details
- Document Type
- DoD Grant Award
- Publication Date
- Feb 06, 2017
- Source ID
- FA95501710060
Entities
People
- Alexander Wagner
Organizations
- Air Force Office of Scientific Research
- German Aerospace Center
- United States Air Force