Contoured nozzle design and evaluation for hotshot wind tunnels
- 8 April 1968
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- A METHOD OF CALCULATING TURBULENT-BOUNDARY-LAYER GROWTH AT HYPERSONIC MACH NUMBERSPublished by Defense Technical Information Center (DTIC) ,1959