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Flat plate cascades at supersonic speed
- Author / Creator
- Available as
- Online
- Summary
-
A brief review of exact two-dimensional supersonic flow theory and Ackeret's linearized theory are first presented. The lift and drag coefficients of a cascade of flat plates are calculated exactly...
A brief review of exact two-dimensional supersonic flow theory and Ackeret's linearized theory are first presented. The lift and drag coefficients of a cascade of flat plates are calculated exactly and compared to those obtained using the linearized theory. The forces on the cascade are determined for unsteady inlet flow. The flat plate cascade theory is extended to compute the efficiency of a supersonic propeller with friction and finite blade thickness.
Details
- Creator
- by Rashad M. El Badrawy
- Format
- Books
- Language
- English
- Publication
-
- Washington, D.C. : National Advisory Committee for Aeronautics, 1956
- Physical Details
-
- 1 online resource (iii, 130 pages) : illustrations, tables, photographs
- data file
- OCLC
- on1382585029
- Date of issue: May 1956.
- Report no. NACA-TM-1369.
- "Translated from Mitteilungen aus dem Institut fur Aerodynamik an der E.T.H. No. 19, 1952, by the National Advisory Committee for Aeronautics"
- Title from title screen (viewed June 9, 2023)
- Includes bibliographical references (page 78)
- Electronic reproduction. Denton, Texas : University of North Texas, 2011. Electronic reproduction from print master produced by University of North Texas.