Effect of Propeller Slipstream on Heat-Exchanger Installations at Low Reynolds Number
- 1 July 2003
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 40 (4) , 751-758
- https://doi.org/10.2514/2.3154
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Experimental investigation of the effect of propeller slipstream on boundary layer behavior at low Reynolds numberPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2000
- Aerodynamics of heat exchangers for high-altitude aircraftPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1995
- Hot-Wire AnemometryPublished by Oxford University Press (OUP) ,1995
- Effects of Small-Scale, High Intensity Inlet Turbulence on Flow in a Two-Dimensional DiffuserJournal of Fluids Engineering, 1984
- Effects of Free-Stream Turbulence on Diffuser PerformanceJournal of Fluids Engineering, 1981
- Improving Diffuser Performance by Artificial MeansAIAA Journal, 1972