Aerodynamics of horizontally-opposed aircraft engine installations
Author:
Affiliation:
1. (Mississippi State University, Mississippi State, Miss.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1977-1249
Reference8 articles.
1. R u b e r t , K. E'. and Knopf, 6 . S. "A Method f o r t h e Design of Cooling Systems f a r A i r c r a f t Power-Plant I n s t a l l a t i o n s , '' NACA Wartime Report L-491, 1942.
Cited by 5 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Effect of Propeller on Engine Cooling System Drag and Performance;Journal of Aircraft;1982-03
2. Full-scale Wind-Tunnel Study of the Effect of Nacelle Shape on Cooling Drag;Journal of Aircraft;1981-02
3. Effect of propeller slipstream on the drag and performance of the engine cooling system for a general aviation twin-engine aircraft;Aircraft Systems Meeting;1980-08-04
4. Study of cooling air inlet and exit geometries for horizontally opposed piston aircraft engines;16th Joint Propulsion Conference;1980-06-30
5. Full-scale wind tunnel study of nacelle shape on cooling drag;Aircraft Systems and Technology Meeting;1979-08-17
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