Steady Expansion of Shock-Heated Gases for Recombination Studies
- 1 May 1969
- journal article
- Published by AIP Publishing in Physics of Fluids
- Vol. 12 (5), I-113-113
- https://doi.org/10.1063/1.1692588
Abstract
An analysis has been undertaken of the conditions for which Wilson's technique involving the steady Prandtl‐Meyer expansion of shock‐heated gases is applicable. Experimental evidence for the predicted flow regimes is described, including measurements of static pressure, stagnation point heat transfer, infrared emission and optical absorption. Work involving iodine recombination is mentioned briefly.Keywords
This publication has 8 references indexed in Scilit:
- Aeronautical Research at the University of SouthamptonJournal of the Royal Aeronautical Society, 1965
- EFFECTS OF EXHAUST NOZZLE RECOMBINATION ON HYPERSONIC RAMJET PERFORMANCEAIAA Journal, 1963
- Structure of a Prandtl-Meyer Expansion in an Ideal Dissociating GasPhysics of Fluids, 1963
- Direct Measurements of Recombination Rates in a Shock TubePhysics of Fluids, 1963
- An experiment to measure the recombination rate of oxygenJournal of Fluid Mechanics, 1963
- O 2 Vibration Relaxation in Oxygen-Argon MixturesThe Journal of Chemical Physics, 1961
- Vibrational relaxation in oxygen and nitrogenJournal of Fluid Mechanics, 1956
- Shock waves in chemical kinetics. The rate of dissociation of molecular iodineDiscussions of the Faraday Society, 1954