The effect of cooling passage aspect ratio on curvature heat transfer enhancement
By: Michael L. Meyer.
Contributors: Lewis Research Center.
Series: NASA technical memorandum -- 107426.
Publisher: National Aeronautics and Space Administration, Lewis Research Center; National Technical Information Service, distributor
Published: 1997
Place of publication: [Cleveland, Ohio]; [Springfield, Va
Language: eng
Format: Microform
Number of pages: 16
Subjects: Rocket engines -- Cooling.; Heat -- Convection.; Convective heat transfer.; Heat transfer coefficients.; Rocket engine design.; Resistive heating.; Curvature.; High aspect ratio.; Secondary flow.
Notes: Shipping list no.: 1997-0768-M.

"March 1997."

Includes bibliographical references (p. 7-8).

Also available via Internet from the NASA Web site. Address as of 9/09/04: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19970012643%5F1997021375.pdf; current access available via PURL.

Microfiche. [Washington, D.C.] : Supt. of Docs., U.S. G.P.O., [1997] 1 microfiche : negative.