Opening book details…
About this book
Validation of a computer code for analysis of subsonic aerodynamic performance of wings with flaps in combination with a canard or horizontal tail and an application to optimization by Carlson, Harry W. is a book available to read on EtoBox.
- Author
- Carlson, Harry W.
- Publisher
- National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; For sale by the National Technical Information Service, 1990.
- Published
- 1990
- Language
- EN
More by Carlson, Harry W.
Browse all works by Carlson, Harry W.
Similar books
- Two Dimensional Aerodynamic Interference Effects on Oscillating Airfoils with Flaps in Ventilated Subsonic Wind Tunnels / Joseph Fromme, Michael Golberg, and John Werth. — Fromme, Joseph. (1979)
- Low-speed Static Lateral Stability Characteristics of a Canard Model Having a 60° Triangular Wing and Horizontal Tail — William R. Bates (1949)
- Applicability of Linearized-theory Attached-flow Methods to Design and Analysis of Flap Systems at Low Speeds for Thin Swept Wings with Sharp Leading Edges / Harry W. Carlson, Christine M. Darden. — Harry W. Carlson (1987)
- Subsonic Kernel-function Flutter Analysis of a Highly Tapered Tail Surface and Comparison with Experimental Results — Gerald D. Walberg (1962)
- Effectiveness of an All-movable Horizontal Tail on an Unswept-wing and Body Combination for Mach Numbers from 0.60 to 1.40 — Louis S. Stivers (1959)
- Numerical Investigation of Aerodynamics of Canard-controlled Missile Using Planar and Grid Tail Fins. Part II, Subsonic and Transonic Flow — DeSpirito, James, (2004)