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A flight investigation of the practical problems associated with porous-leading-edge suction
- Author / Creator
- Available as
- Online
- Summary
-
A flight investigation has been made of the practical problems associated with the use of porous-leading-edge suction. The wing leading edge of the test airplane was porous over approximately 83 pe...
A flight investigation has been made of the practical problems associated with the use of porous-leading-edge suction. The wing leading edge of the test airplane was porous over approximately 83 percent of the span and the first 8 percent of the chord of the upper surface. Various other extents of suction area within these limits were also tested.
Details
- Creator
- by Paul A. Hunter
- Format
- Books
- Language
- English
- Contributors
- Publication
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- Washington, D.C. : National Advisory Committee for Aeronautics, 1954
- Physical Details
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- 1 online resource (42 pages) : illustrations, tables, photographs
- data file
- OCLC
- on1374333576
- Title from title screen (viewed March 13, 2023)
- Date of issue: February 1954.
- Report no. NACA-TN-3062.
- "Langley Aeronautical Laboratory.⁰́₊
- Includes bibliographical references (page 16)
- Electronic reproduction. Denton, Texas : University of North Texas, 2011. Electronic reproduction from print master produced by University of North Texas.