Design and Performance of a Simple Interferometer for Wind-Tunnel Measurements
- 1 February 1951
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 18 (2) , 82-90
- https://doi.org/10.2514/8.1862
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- The Shock Tube: A Facility for Investigations in Fluid DynamicsReview of Scientific Instruments, 1949
- Interferometric Studies of Faster than Sound Phenomena. Part I. The Gas Flow around Various Objects in a Free, Homogeneous, Supersonic Air StreamPhysical Review B, 1948
- The Interaction Between Boundary Layer and Shock Waves in Transonic FlowJournal of the Aeronautical Sciences, 1946
- An optical method for measuring temperature distribution and convective heat transferBureau of Standards Journal of Research, 1932