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Numerical determination of indicial lift and moment functions for a two-dimensional sinking and pitching airfoil at Mach numbers 0.5 and 0.6
- Author / Creator
- Available as
- Online
- Summary
-
Approximate values for the indicial lift and moment functions on a sinking and pitching airfoil are calculated for Mach numbers of 0.5 and o.6. The indicial lift function associated with an airfoil...
Approximate values for the indicial lift and moment functions on a sinking and pitching airfoil are calculated for Mach numbers of 0.5 and o.6. The indicial lift function associated with an airfoil penetrating a sharp-edge gust is also determined approximately at Mach numberes 0.5, 0.6, and 0.7.
Details
- Creator
- by Bernard Mazelsky and Joseph A. Drischler
- Format
- Books
- Language
- English
- Contributors
- Publication
-
- Washington, D.C. : National Advisory Committee for Aeronautics, 1952
- Physical Details
-
- 1 online resource (37 pages) : illustrations, tables
- data file
- OCLC
- on1362884745
- Title from title screen (viewed December 2, 2022)
- Date of issue: July 1952.
- Report no. NACA-TN-2739.
- "Langley Aeronautical Laboratory."
- Includes bibliographical references(page 23)
- Electronic reproduction. Denton, Texas : University of North Texas, 2011. Electronic reproduction from print master produced by University of North Texas.