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The pressure distribution over a modified elliptical wing tip on a biplane in flight / by Richard V. Rhode and Eugene E. Lundquist.
- Format:
- Book
- Government document
- Author/Creator:
- Rhode, Richard V., author.
- Lundquist, Eugene E., author.
- Series:
- Technical note (United States. National Advisory Committee for Aeronautics) ; 387.
- Technical note / National Advisory Committee for Aeronautics ; No. 387
- Language:
- English
- Subjects (All):
- Biplanes.
- Airplanes--Wings.
- Airplanes.
- Aerodynamic load--Testing.
- Aerodynamic load.
- biplanes.
- Physical Description:
- 1 online resource (14 pages, 8 unnumbered pages) : illustrations.
- Place of Publication:
- Washington, [D.C.] : National Advisory Committee for Aeronautics, 1931.
- Summary:
- This note presents the results of flight pressure distribution tests on the right upper wing panel of a Douglas M-3 airplane equipped with a modified elliptical tip having a slight amount of washout.
- The results are given in tables and curves in such form that the load distribution for any normal force coefficient within the usual range encountered in flight may be determined.
- Notes:
- Title from title screen (viewed February 5, 2020).
- "August, 1931."
- "Langley Memorial Aeronautical Laboratory."
- No Federal Depository Library Program (FDLP) item number.
- Includes bibliographical references (page 4).
- Electronic reproduction. Denton, Texas : University of North Texas, 2011. Electronic reproduction from print master produced by University of North Texas.
- Other Format:
- Print version: Rhode, Richard V. The pressure distribution over a modified elliptical wing tip on a biplane in flight
- OCLC:
- 1139565335
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