Extension to an analysis of turbulent swirling compressible flow for application to axisymmetric small gas turbine ducts
By: O.L. Anderson, G.B. Hankins, D.E. Edwards ; prepared for National Aeronautics and Space Administration, Lewis Research Center for U.S. Department of Energy, Conservation and Solar Energy, Office of Transportation Programs under interagency agreement DE-AI01-77C551040
Contributors: Hankins, G. B; Edwards, D. E; Lewis Research Center; United Technologies Research Center; United States. Dept. of Energy. Office of Transportation Programs
Series: NASA CR -- 165597; NASA contractor report -- 165597
Publisher: The Center; For sale by the National Technical Information Service
Published: 1982
Place of publication: Cleveland, Ohio; [Springfield, Va
Language: eng
Format: Microform
Subjects: Turbulent boundary layer
Notes: Microfiche. [Washington, D.C. : NASA, 1984]. 1 microfiche ; 11 x 15 cm

"United Technologies Research Center."

"February 1982."

"DOE/NASA/0235-1."

"UTRC-915395-12."

"N84-21445"--Microfiche header

Includes bibliographical references

Nov. 1980-Nov. 1981

DEN3-235