Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Reference8 articles.
1. Tecnical Notes
2. Truncated Perfect Nozzles in Optimum Nozzle Design
3. Courant, R. and Friedrics, K. O., Supersonic Flow and Shock Waves (Interscience Publishers Inc., New York,1948), pp.57-58.