A further note on shock-tube measurements of end-wall radiative heattransfer in air
- 1 November 1969
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 7 (11), 2170-2172
- https://doi.org/10.2514/3.5586
Abstract
No abstract availableKeywords
This publication has 8 references indexed in Scilit:
- BOUNDARY INTERFERENCE AT SUBSONIC SPEEDS IN WIND TUNNELS WITH VENTILATED WALLSPublished by Defense Technical Information Center (DTIC) ,1969
- Shock-tube measurements of end-wall radiative heat transfer in air.AIAA Journal, 1968
- Radiative Transfer Effects on the Flow Field and Heat Transfer behind a Reflected Shock Wave in AirPhysics of Fluids, 1967
- Atomic transition probabilities :Published by National Institute of Standards and Technology (NIST) ,1966
- Shock-tube studies of equilibrium air radiationAIAA Journal, 1965
- Apparent positions of photoelectric edges and the merging of spectrum linesJournal of Quantitative Spectroscopy and Radiative Transfer, 1964
- The Upwash Correction for an Oscillating Wing in a Wind TunnelJournal of the Aeronautical Sciences, 1953
- On the Compressibility Correction for Subsonic Unsteady FlowJournal of the Aeronautical Sciences, 1950