Subsonic cascade wind tunnel tests of a sundstrand controlled-diffusion fan blade section
By: [by] A.G. McGuire and R.P. Shreeve
Contributors: Shreeve, R. P.; Naval Postgraduate School (U.S.)
Publisher: Naval Postgraduate School
Published: 1984
Place of publication: Monterey, California
Language: eng
Number of pages: 59
Subjects: Wind tunnel testing; Fluid mechanics
Description: Results are given of subsonic cascade wind tunnel tests of a controlled diffusion fan blade section designed by Sundstrand Corporation.  Data were obtained successfully at air inlet angles less than and approaching design incidence.  Operation at design and higher incidence angles would require side wall suction.  It was concluded that the design was successful and that a fan test should be considered.
Notes: Title from cover.

"Prepared for: Sundstrand Aviation Operations"--Cover.

"December 1984"--Cover.

"NPS-67-84-021PR"--Cover.

Author(s) key words: Controlled diffusion, fan blade design, cascade wind tunnel.

Includes bibliographical references (p. 58).

Technical report; 1984.

kmc/kmc 10/23/09.