The Effects of leading edge and downstream film cooling on turbine vane heat transfer
By: L.D. Hylton ... [et al.].
Contributors: Hylton, L. D.; United States. National Aeronautics and Space Administration.
Series: Allison EDR -- 13481.; NASA contractor report -- 182133.; NASA contractor report -- NASA CR-182133.
Publisher: National Aeronautics and Space Administration
Published: 1989
Place of publication: [Washington, DC]
Language: eng
Format: Microform
Subjects: Aerofoils.; Heat -- Transmission.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1989. 2 microfiches.