A method of characteristics approach to the problem of supersonic flow past oscillating cascades with finite blade thickness
By: by K. Vogeler
Contributors: Naval Postgraduate School (U.S.)
Publisher: Naval Postgraduate School
Published: 1978
Place of publication: Monterey, Calif
Language: eng
Number of pages: 153
Subjects: Turbomachines; Aerodynamics; Cascades (Fluid dynamics); Fluid dynamics; Blades
Description: A method of characteristics approach is described for the computation of supersonic flow past oscillating cascades having blades of finite thickness distribution. The transonic small disturbance equation is solved for cascades with subsonic leading-edge locus. Sample calculations are presented for the inlet and passage flow and comparisons are given with calculations for flat-plate cascades and available measured pressure distributions. (Author)
Notes: Title from cover.

"Prepared for: Chief of Naval Research"--Cover.

"October 1978"--Cover.

"NPS-67-78-012"--Cover.

Includes bibliographical references (p. 152-153)

"Approved for public release; distribution unlimited"--Cover.

Technical report; 1978.