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Aerodynamic characteristics and flap loads of the brake-flap installation on the 0.40-scale model of the F4F-3 left wing panel
- Author / Creator
- Available as
- Online
- Summary
-
Tests have been made in the LMAL 7- by 10-foot tunnel for determining the aerodynamic characteristics and the flap loads of a brake-flap installation on a 0.40-scale semispan model of the F4F-3 lef...
Tests have been made in the LMAL 7- by 10-foot tunnel for determining the aerodynamic characteristics and the flap loads of a brake-flap installation on a 0.40-scale semispan model of the F4F-3 left wing panel. The data presented in coefficient form and include lift, drag, and pitching-moment coefficients of the airfoil-flap combinations and the normal-force, chord-force, and hinge-moment coefficients of the upper (perforated split) flap and the lower (slotted) flap.
Details
- Creator
- by Paul E. Purser and Robert B. Liddell
- Format
- Books
- Language
- English
- Contributors
- Publication
-
- Washington, D.C. : National Advisory Committee for Aeronautics, 1942
- Physical Details
-
- 1 online resource (14, [37] pages) : illustrations, tables, photographs
- data file
- OCLC
- on1444262582
- Title from title screen (viewed July 9, 2024)
- Date of issue: October 1942.
- NACA Wartime Report L-549.
- Originally issued as NACA as a Memorandum Report.
- Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia.
- Includes bibliographical references (pages 13-14)
- Electronic reproduction. Denton, Texas : University of North Texas, 2011. Electronic reproduction from print master produced by University of North Texas.
Subjects
- Airplanes -- Models -- Wings.
- Airplanes -- Control.
- Flaps (Airplanes)
- Aerodynamic load.
- Charts, diagrams, etc.
- diagrams.
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