Aerodynamic Characteristics of a Series of Bodies with and without Tails at Mach Numbers from 0.8 to 3.0 and Angles of Attack from 0 to 45 degrees.
Jimmie N. Derrick, D. J. Spring, G. C. Winn
Abstract
Jimmie N. Derrick, D. J. Spring, G. C. Winn
Abstract
Wind tunnel tests were conducted in a 16 ft. transonic tunnel, a supersonic tunnel, A and a trisonic tunnel to establish a bank of systematic data for body and body-tail configurations at high angles of attack. The configurations were tested at Mach numbers between 0.8 and 3.0, angles of attack from -2 to 45 degrees, and roll angles from 0 to 90 degrees. The aerodynamic characteristics were obtained for the total configuration as well as each of the four undeflected tail fins.
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Wind tunnel tests were conducted in a 16 ft. transonic tunnel, a supersonic tunnel, A and a trisonic tunnel to establish a bank of systematic data for body and body-tail configurations at high angles of attack. The configurations were tested at Mach numbers between 0.8 and 3.0, angles of attack from -2 to 45 degrees, and roll angles from 0 to 90 degrees. The aerodynamic characteristics were obtained for the total configuration as well as each of the four undeflected tail fins.
Key concepts: Mach number, Transonic, Supersonic speed, Aerodynamics, Wind tunnel, Supersonic wind tunnel, Angle of attack, Series (stratigraphy)