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 PDF Download
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Author: Jimmie N. Derrick Publisher: ISBN: Category : Aerodynamics, Transonic Languages : en Pages : 896
Book Description
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.
Author: Jimmie N. Derrick Publisher: ISBN: Category : Aerodynamics, Transonic Languages : en Pages : 896
Book Description
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.
Author: Publisher: ISBN: Category : Aeronautics Languages : en Pages : 756
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Author: Jimmie N. Derrick
Author: Jimmie N. Derrick
Author: 
Author: William B. Baker (Jr.)
Author: Frank Moore
Author: United States. National Aeronautics and Space Administration
Author: James F. Campbell
Author: 
Author: United States. National Aeronautics and Space Administration
Author: United States. National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics