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The effects of a highly cambered low-drag wing and of auxiliary flaps on the high-speed aerodynamic characteristics of a twin-engine pursuit airplane model
- Author / Creator
- Available as
- Online
- Summary
-
Results are presented for tests of two wings, an NACA 230-series wing and a highly-cambered NACA 66-series wing on a twin-engine pursuit airplane. Auxiliary control flaps were tested in combination...
Results are presented for tests of two wings, an NACA 230-series wing and a highly-cambered NACA 66-series wing on a twin-engine pursuit airplane. Auxiliary control flaps were tested in combinations with each wing. Data showing comparison of high-speed aerodynamic characteristics of the model when equipped with each wing, the effect of the auxiliary control flaps on aerodynamic characteristics, and elevator effectiveness for the model with the 66-series wing are presented. High-speed aerodynamic characteristics of the model were improved with the 66-series wing.
Details
- Creator
- by Victor M. Ganzer
- Format
- Books
- Language
- English
- Publication
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- Washington, D.C. : National Advisory Committee for Aeronautics, 1944
- Physical Details
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- 1 online resource (12, [46] pages) : illustrations, photographs
- data file
- OCLC
- on1409340021
- Title from title screen (viewed November 14, 2023)
- Date of issue: February 1944.
- NACA Wartime Report A-90.
- Originally issued as NACA as a Memorandum Report.
- Prepared at the Ames Aeronautical Laboratory, Moffett Field, California.
- Report numbers NACA-WR-A-90.
- Includes bibliographical references (page 12)
- Electronic reproduction. Denton, Texas : University of North Texas, 2011. Electronic reproduction from print master produced by University of North Texas.