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EJECTION COOLING OF THE XR-10 HELICOPTER POWER PLANT
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English
Abstract
This paper discusses the problems involved in the design and development of an ejector cooling system for the XR-10 Helicopter power plant. Basic design problems are reviewed. Test experience on exhaust stacks, nozzles, mixing chambers, diffusers, baffles, carburetors and engines are discussed in detail.
Authors
Citation
DOUGLAS, L., "EJECTION COOLING OF THE XR-10 HELICOPTER POWER PLANT," SAE Technical Paper 470013, 1947, https://doi.org/10.4271/470013.Also In
References
- XR-10 Cooling Survey Kellett Report No. 1260.3 July 1946
- Collins Bachle Preliminary Investigation of the Use of Exhaust Gas Ejectors For Engine Cooling Continental Aviation and Engineering Corp. Report No. 273 July 1944
- Campbell Tests of Exhaust Propulsion Nozzles United Aircraft Corporation Report No. R-309 December 1942
- McClintock Theoretical Calculations of Steady-Flow Ejector Performance United Aircraft Corp. Report No. R-447 May 1944
- Kittredge Preliminary Flight Investigations of Exhaust Jet Augmentor Performance in Single Place “Hawk” Airplane Wright Aeronautical Corp. Report No. 1106 February 1947
- Marquardt A Theoretical and Experimental Investigation of Exhaust Ejectors for Cooling at Low Speeds NACA Advanced Confidential Report
- Pinkel NACA Study of the Utilization of Exhaust Gas of Aircraft Engines April 1946
- Pinkel Turner Voss Design of Nozzles for the Individual Cylinder Exhaust Jet Propulsion System NACA, ACR April 1941
- Bierman Cook Held Improving Engine Cooling With Special Baffles NACA ARR E5B05 February 1945
- Mangamello Bogatsky An Experimental Investigation of Rectangular Gas Ejectors Applicable for Engine Cooling NACA ARR E4E31 May 1944
- Pinkel Heat Transfer Processes in Air Cooled Engine Cylinders NACA Rep. #612 1938