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Application of High-Temperature Materials to Aircraft Powerplants in the Temperature Range 12002400 F Marquardt Aircraft Company
- Format:
- Conference/Event
- Author/Creator:
- Levy, Alan V., author.
- Conference Name:
- Aircraft Research Seminar held by the SAE Southern California Section at the University of California
- Language:
- English
- Physical Description:
- 1 online resource
- Place of Publication:
- Warrendale, PA SAE International 1956
- Summary:
- OUR aircraft industry is fast approaching the time when it will be hard-pressed to design and construct elevated-temperature structural components from engineering materials now available. This situation is particularly aggravated in afterburner, ramjet, and rocket engine design, where operating combustion temperatures may exceed the melting points of constructional metals developed to date.Several applications of available alloys to combustion-chamber design are described, and it is concluded that new materials such as molybdenum, cermets, and ceramic coatings, together with refined cooling techniques, must provide the answer to the limitations imposed by the inadequacies of elevated-temperature materials available today
- Notes:
- Vendor supplied data
- Publisher Number:
- 560035
- Access Restriction:
- Restricted for use by site license
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