Search

Search Constraints

Start Over You searched for: Publish Year Decade 1950 - 1959 Remove constraint Publish Year Decade: 1950 - 1959 Catalog Issue Year Decade 1960 - 1969 Remove constraint Catalog Issue Year Decade: 1960 - 1969

Search Results

389. NACA research memorandum RM (series). A57H19. Effects of leading-edge slat and trailing-edge split flap on aerodynamic characteristics of wing-fuselage combination having nearly triangular wing of aspect ratio 2.9 at Mach numbers from 0.60 to 0.92 [with list of references]; by Fred A. Demele.