Opening book details…
About this book
Characteristics at Mach Number of 2.03 of a Series of Wings Having Various Spanwise Distributions of Thickness Ration and Chord by Robins, A. Warner. is a book available to read on EtoBox.
- Author
- Robins, A. Warner.
- Publisher
- National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1960]
- Published
- 1960
- Language
- EN
More by Robins, A. Warner.
Browse all works by Robins, A. Warner.
Similar books
- Investigation of the Aerodynamic Characteristics at High Supersonic Mach Numbers of a Family of Delta Wings Having Double-wedge Sections with the Maximum Thickness at 0.18 Chord / Mitchel H. Bertram and William D. McCauley. — Mitchel H. Bertram (1954)
- Effect of Thickness, Camber, and Thickness Distribution on Airfoil Characteristics at Mach Numbers Up to 1.0 / Bernard N. Daley and Richard S. Dick. — Bernard N. Daley (1952)
- Thickness-dependent Characteristics and Oxidation of 2D-cadmium — Arda Gulucu & Hasan Sahin
- Experimental Investigation of an Axial-flow Supersonic Compressor Having Sharp Leading-edge Blades with an 8-Percent Mean Thickness-chord Ratio — Theodore J. Goldberg (1955)
- Experimental Pressure Distributions Over Two Wing-body Combinations at Mach Number 1.9 — Moskowitz, Barry. (1951)
- Transonic Flutter Characteristics of a 45° Sweptback Wing with Various Distributions of Ballast Along the Leading Edge — John R. Unangst (1959)