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Installation Effects on the CF6-50 in the YC-14 Aircraft
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English
Abstract
Design of the YC-14 over-the-wing nacelle, utilizing the CF6-50D engines, presented unique engine installation conditions which have been accommodated with very minor impact to the baseline commercial engine design. Major installation features which affect the engine are reviewed including engine mounting, engine/aircraft deflections and nacelle sealing, effect of the confluent-flow exhaust nozzle on engine cycle matching, and inlet/thrust reverser/engine compatibility. Design solutions and planned testing to evaluate the installation are discussed.
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Citation
Tuten, R., Housley, F., and Hess, P., "Installation Effects on the CF6-50 in the YC-14 Aircraft," SAE Technical Paper 750607, 1975, https://doi.org/10.4271/750607.Also In
References
- Foody James J. “The Air Force/Boeing Advanced Medium STOL Transport Prototype.” Paper 730365 SAE National Air Transportation Meeting Miami April 1973
- Wimpress John K. “Upper Surface Blowing Technology as Applied to the YC-14 Airplane.” Paper 730916 SAE National Aerospace Meeting Los Angeles October 1973
- Skavdahl Howard “Nozzle Development for the Upper Surface Blown Jet Flap on the YC-14 Airplane.” Paper 740469 SAE National Air Transportation Meeting Dallas April 1974
- Kimes Lucas J. “YC-14 Engine Installation Features.” AIAA Paper No. 74-972 August 12-14 1974