Comparison of high aspect ratio cooling channel designs for a rocket combustion chamber with development of an optimized design / by Mary F. Wadel.

Author/creator Wadel, Mary F. author.
Other author Lewis Research Center, issuing body.
Format Electronic
PublicationCleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, January 1998.
Description1 online resource (approximately 78 pages) : illustrations.
Supplemental Contenthttps://purl.fdlp.gov/GPO/gpo174895

SeriesNASA/TM ; 1998-206313
NASA technical memorandum ; 1998-206313. ^A467613
General note"January 1998."
General noteGPO Cataloging Record Distribution Program (CRDP).
Bibliography noteIncludes bibliographical references (pages 67-69).
Report noteTechnical memorandum.
Source of descriptionDescription based on online resource, PDF version; title from title page (NASA, viewed on Feb. 14, 2022).
Issued in other formPrint version: Wadel, Mary F Comparison of high aspect ratio cooling channel designs for a rocket combustion chamber with development of an optimized design
Genre/formAcademic theses.
GPO item number0830-D (online)
Govt. docs number NAS 1.15:1998-206313

Availability

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Electronic Resources Access Content Online ✔ Available