Boundary layer effects on density measurements in shock tubes
- 15 May 1976
- journal article
- letter
- Published by AIP Publishing in The Journal of Chemical Physics
- Vol. 64 (10) , 4233-4234
- https://doi.org/10.1063/1.431999
Abstract
No abstract availableKeywords
This publication has 20 references indexed in Scilit:
- Vibrational relaxation in carbon dioxide with selected collision partners. I. Water and heavy waterThe Journal of Physical Chemistry, 1972
- Density Gradient Measurements of O2 Dissociation in Shock WavesThe Journal of Chemical Physics, 1971
- Vibrational Energy Transfer in Shock-Heated N2–HI and N2–DI MixturesThe Journal of Chemical Physics, 1971
- Shock Tube Technique in Chemical KineticsAnnual Review of Physical Chemistry, 1969
- Flow Field behind a Shock Wave in a Low-Pressure Test GasPhysics of Fluids, 1969
- Relaxation Processes in Shock WavesPublished by Springer Nature ,1967
- Series solutions for shock tube laminar boundary layer and test time.AIAA Journal, 1966
- Shock Front Curvature at Initial Pressures up to 700 mm HgPhysics of Fluids, 1966
- Shock tube test time limitation due to turbulentwall boundary layerAIAA Journal, 1964
- On the stability of plane shock wavesJournal of Fluid Mechanics, 1957