NDLI: Development and fabrication of structural components for a scramjet engine

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Development and fabrication of structural components for a scramjet engine

Content Provider	NASA Technical Reports Server (NTRS)
Author	Buchmann, O. A.
Copyright Year	1990
Description	A program broadly directed toward design and development of long-life (100 hours and 1,000 cycles with a goal of 1,000 hours and 10,000 cycles) hydrogen-cooled structures for application to scramjets is presented. Previous phases of the program resulted in an overall engine design and analytical and experimental characterization of selected candidate materials and concepts. The latter efforts indicated that the basic life goals for the program can be reached with available means. The main objective of this effort was an integrated, experimental evaluation of the results of the previous program phases. The fuel injection strut was selected for this purpose, including fabrication development and fabrication of a full-scale strut. Testing of the completed strut was to be performed in a NASA-Langley wind tunnel. In addition, conceptual designs were formulated for a heat transfer test unit and a flat panel structural test unit. Tooling and fabrication procedures required to fabricate the strut were developed, and fabrication and delivery to NASA of all strut components, including major subassemblies, were completed.
File Size	18326900
Page Count	244
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19900010772
Archival Resource Key	ark:/13960/t3130sb1f
Language	English
Publisher Date	1990-03-01
Access Restriction	Open
Subject Keyword	Aircraft Propulsion And Power Fabrication Structural Design Thermal Protection Engine Design Supersonic Combustion Ramjet Engines Wind Tunnel Tests Struts Subassemblies Fuel Injection Heat Transfer Regenerative Cooling Tooling Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Technical Report

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