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Low-speed characteristics of four cambered, 10-percent-thick NACA airfoil sections
- Author / Creator
- Available as
- Online
- Summary
-
Low-speed lift, drag, and pitching-moment characteristics have been obtained for 10-percent-thick sections of the NACA four-digit- and 64A-series airfoil sections, each cambered with the same a-typ...
Low-speed lift, drag, and pitching-moment characteristics have been obtained for 10-percent-thick sections of the NACA four-digit- and 64A-series airfoil sections, each cambered with the same a-type mean line for design lift coefficients of both 0.3 and 0.8. The NACA fouyr-digit-series sections achieved greater values of maximum lift than did the corresponding NACA 64A-series sections, but this superiority was less marked for the more highly cambered sections.
Details
- Creator
- by George B. McCullough and William M. Haire
- Format
- Books
- Language
- English
- Contributors
- Publication
-
- Washington, D.C. : National Advisory Committee for Aeronautics, 1950
- Physical Details
-
- 1 online resource (25 pages) : illustrations, tables ; 28 cm
- data file
- OCLC
- on1295697534
- Title from title screen (viewed February 8, 2022)
- "Ames Aeronautical Laboratory.⁰́₊
- Date of issue: August 1950.
- Report no. NACA-TN-2177.
- Includes bibliographical references.
- Electronic reproduction. Denton, Texas : University of North Texas, 2011. Electronic reproduction from print master produced by University of North Texas.