Series solutions for shock tube laminar boundary layer and test time.
- 1 May 1966
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 4 (5), 782-789
- https://doi.org/10.2514/3.3547
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Measurements of test time in the galcit 17-inch shock tubeAIAA Journal, 1964
- Shock tube test time limitation due to turbulentwall boundary layerAIAA Journal, 1964
- Test Time in Low-Pressure Shock TubesPhysics of Fluids, 1963
- On Flow Duration in Low-Pressure Shock TubesPhysics of Fluids, 1960
- Shock-Tube Performance at Low Initial PressurePhysics of Fluids, 1959
- The Transverse Curvature Effect in Compressible Axially Symmetric Laminar Boundary-Layer FlowJournal of the Aeronautical Sciences, 1956