Experimental study of high-enthalpy shock- tunnel flow. I - Shock-tube flow and nozzle starting time.
- 1 August 1969
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 7 (8) , 1553-1560
- https://doi.org/10.2514/3.5431
Abstract
No abstract availableThis publication has 11 references indexed in Scilit:
- An investigation of the reflected shock interaction process in a shock tube.AIAA Journal, 1968
- Effects of interface combustion and mixing on shock-tunnel conditionsAIAA Journal, 1964
- Shock tube test time limitation due to turbulentwall boundary layerAIAA Journal, 1964
- Test Time in Low-Pressure Shock TubesPhysics of Fluids, 1963
- Experimental Investigation of the Equilibrium Interface TechniquePhysics of Fluids, 1962
- Testing Time and Contact-Zone Phenomena in Shock-Tube FlowsPhysics of Fluids, 1961
- On Flow Duration in Low-Pressure Shock TubesPhysics of Fluids, 1960
- Boundary-Layer Transition and Heat Transfer in Shock TubesJournal of the Aerospace Sciences, 1960
- Shock-Tube Performance at Low Initial PressurePhysics of Fluids, 1959
- Shock-Tube Testing TimeJournal of the Aerospace Sciences, 1959