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Flight investigation of the effect of a local change in wing contour on chordwise pressure distribution at high speeds
- Author / Creator
- Available as
- Online
- Summary
-
Tests were made in high-speed flight with a fighter airplane to determine the effect of the chordwise pressure distribution resulting from a minor modification in the contour of the wing upper surf...
Tests were made in high-speed flight with a fighter airplane to determine the effect of the chordwise pressure distribution resulting from a minor modification in the contour of the wing upper surface.
Details
- Creator
- by Richard E. Adams and Norman S. Silsby
- Included Title
-
- Technical Report Archive & Image Library (TRAIL)
- Format
- Books
- Language
- English
- Contributors
- Publication
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- Washington, D.C. : National Advisory Committee for Aeronautics, 1946
- Physical Details
-
- 1 online resource (5, [7] pages) : illustrations
- data file
- OCLC
- on1200353473
- "Langley Memorial Aeronautical Laboratory."
- Title from title screen (viewed October 13, 2020)
- Date of issue: September 1946.
- Report no. NACA-TN-1152.
- Includes bibliographical references (page 5)
- Electronic reproduction. Denton, Texas : University of North Texas, 2011. Electronic reproduction from print master produced by University of North Texas.