Website Search
Find information on spaces, staff, and services.
Catalog Search
Books
Generalized linearized conical flow
- Author / Creator
- Available as
- Online
- Summary
-
A basic theory of generalized linearized supersonic conical flow for both inside and outside the Mach cone was developed and applied to several specific problems including unsteady-flow conditions....
A basic theory of generalized linearized supersonic conical flow for both inside and outside the Mach cone was developed and applied to several specific problems including unsteady-flow conditions. A triangular lifting wing in pitching and rolling with both subsonic and supersonic leading edges was investigated and pressure coefficients were obtained. A family of thin sweptback triangular wings having symmetrical thickness distribution was also investigated and analytic expressions for wave drag and pressure coefficients were determined. Values of wave-drag coefficients were calculated and the results presented graphically.
Details
- Creator
- by W.D. Hayes, R.C. Roberts, and N. Haaser
- Format
- Books
- Language
- English
- Contributors
- Publication
-
- Washington, D.C. : National Advisory Committee for Aeronautics, 1952
- Physical Details
-
- 1 online resource (48 pages) : illustrations, tables
- data file
- OCLC
- on1348187146
- "Brown University."
- Title from title screen (viewed October 18, 2022)
- Date of issue: March 1952.
- Report numbers NACA-TN-2667.
- Includes bibliographical references (page 40)
- Electronic reproduction. Denton, Texas : University of North Texas, 2011. Electronic reproduction from print master produced by University of North Texas.