Results are presented of a wind tunnel investigation conducted at Mach numbers of 0.74 and 1.88 to determine the aerodynamic characteristics of rectangular solid bodies for fineness ratios (FR) of 1, 2, and 3, between 0 and 90 deg angles of attack. All the models had the same frontal area of 1.5 by 1.5 inches. (Author)
Aerodynamic Characteristics of Rectangular Solid Bodies of Various Fineness Ratios at Mach Numbers of 0.74 and 1.88
1967
28 pages
Report
Keine Angabe
Englisch
Fluid Mechanics , Aircraft , Rectangular bodies , External stores , Aerodynamic characteristics , Airframes , Instrumentation , Supersonic flow , Wind tunnel models , Aerodynamic configurations , Angle of attack , Aerodynamic loading , Pitch(Motion) , Lift , Drag , Reduction , Interference , Fines , Ratios , Lift-drag ratio