Effects of rotation on coolant passage heat transfer.
Contributors: Hajek, T. J.; Johnson, B. V.; Wagner, J. H.; Steuber, G. D.; Lewis Research Center.; Pratt & Whitney Company.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Program.
Series: NASA contractor report -- 4396.; NASA contractor report -- NASA CR-4396.
Publisher: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program; Pratt & Whitney; National Technical Information Service, distributor]
Published: 1991
Place of publication: [Washington, D.C.]; East Hartford, Conn; [Springfield, Va
Language: eng
Subjects: Heat -- Transmission; Turbomachines -- Blades -- Cooling
Notes: Shipping list no.: 1992-0323-M (v. 1) and 1994-0071-M (v. 2).

Distributed to depository libraries in microfiche.

"Prepared for Lewis Research Center under contract NAS3-23691."

Also available via Internet from the NTRS web site. Addresses as of 1/31/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19910021175%5F1991021175.pdf (v. 1) and http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19940011518%5F1994011518.pdf (v. 2); current access is available via PURLs.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1991-1994?]. microfiches.
Table of contents: title: v. 1. Coolant passages with smooth walls / T.J. Hajek ... [et al.]; title: v. 2. Coolant passages with trips normal and skewed to the flow / B.V. Johnson, J.H. Wagner, and G.D. Steuber.