Effect of pressure gradient on sonic‐point heat transfer
- 1 January 1968
- journal article
- Published by Wiley in AIChE Journal
- Vol. 14 (1) , 127-134
- https://doi.org/10.1002/aic.690140123
Abstract
No abstract availableKeywords
This publication has 8 references indexed in Scilit:
- Further experiments on transition reversal at hypersonic speeds.AIAA Journal, 1966
- Turbulence determination and blockage correction for immersed cylinder heat transfer at high reynolds numbersAIChE Journal, 1966
- Local heat-transfer coefficients in a nozzle with high-speed laminarflow.AIAA Journal, 1965
- Heat transfer to a turbulent boundary layer with varying free-stream velocity and varying surface temperature—an experimental studyInternational Journal of Heat and Mass Transfer, 1965
- Convective heat transfer in a convergent-divergent nozzleInternational Journal of Heat and Mass Transfer, 1964
- EXPERIMENTAL INVESTIGATION OF HEAT TRANSFER RATES IN ROCKET THRUST CHAMBERSAIAA Journal, 1963
- The Boundary Layer on the End Wall of a Turbine Nozzle CascadeTransactions of the American Society of Mechanical Engineers, 1958
- Convective Heat Transfer to Gas Turbine Blade SurfacesProceedings of the Institution of Mechanical Engineers, 1954