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The effect of split trailing-edge wing flaps on the aerodynamic characteristics of a parasol monoplane / by Rudolf N. Wallace.
Connect to full text Available online
View online- Format:
- Book
- Government document
- Author/Creator:
- Wallace, Rudolf N., author.
- Series:
- Technical note (United States. National Advisory Committee for Aeronautics) ; 475.
- Technical note / National Advisory Committee for Aeronautics ; No. 475
- Language:
- English
- Subjects (All):
- Airplanes--Wings.
- Airplanes.
- Split flaps (Airplanes).
- Wind tunnel testing.
- Physical Description:
- 1 online resource (8 pages, 8 unnumbered pages) : illustrations.
- Place of Publication:
- Washington, [D.C.] : National Advisory Committee for Aeronautics, 1933.
- Notes:
- Title from title screen (viewed March 26, 2020).
- "November, 1933."
- "Langley Memorial Aeronautical Laboratory."
- No Federal Depository Library Program (FDLP) item number.
- Includes bibliographical references (page 7).
- Electronic reproduction. Denton, Texas : University of North Texas, 2011. Electronic reproduction from print master produced by University of North Texas.
- Other Format:
- Print version: Wallace, Rudolf N. The Effect of split trailing-edge wing flaps on the aerodynamic characteristics of a parasol monoplane
- OCLC:
- 1146215375
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