Visualization technique for massive blowing studies.
- 1 July 1966
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 4 (7) , 1305-1307
- https://doi.org/10.2514/3.3667
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- An experimental investigation of stagnation- point injectionJournal of Spacecraft and Rockets, 1965
- The Homogeneous Boundary Layer at an Axisymmetric Stagnation Point With Large Rates of InjectionJournal of the Aerospace Sciences, 1962
- Vibrations of Conical ShellsThe Journal of the Acoustical Society of America, 1960