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Structural design and analysis of a Mach zero to five turbo-ramjet systemThe paper discusses the structural design and analysis of a Mach zero to five turbo-ramjet propulsion system for a Mach five waverider-derived cruise vehicle. The level of analysis detail necessary for a credible conceptual design is shown. The results of a finite-element failure mode sizing analysis for the engine primary structure is presented. The importance of engine/airframe integration is also discussed.
Document ID
19930065833
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Spoth, Kevin A.
(NASA Langley Research Center Hampton, VA, United States)
Moses, Paul L.
(Lockheed Engineering and Sciences Co.; NASA, Langley Research Center Hampton, VA, United States)
Date Acquired
August 16, 2013
Publication Date
June 1, 1993
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AIAA PAPER 93-1983
Meeting Information
Meeting: AIAA, SAE, ASME, and ASEE, Joint Propulsion Conference and Exhibit
Location: Monterey, CA
Country: United States
Start Date: June 28, 1993
End Date: June 30, 1993
Sponsors: ASME, ASEE, AIAA, SAE
Accession Number
93A49830
Funding Number(s)
CONTRACT_GRANT: NAS1-19000
Distribution Limits
Public
Copyright
Other

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