Three-degree-of-freedom Evaluation of the Longitudinal Transfer Functions of a Supersonic Canard Missile Configuration Including Changes in Forward Speed PDF Download
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Author: Ernest C. Seaberg Publisher: ISBN: Category : Aerodynamics, Supersonic Languages : en Pages : 36
Book Description
A reevaluation of existing flight data obtained for a supersonic canard missile configuration of the boost-glide type has been made to determine derivatives not previously evaluated. These derivatives, together with those previously evaluated and published, have been utilized to determine some typical airframe frequency responses based on the three-degree-of-freedom longitudinal equations of motion.
Author: Ernest C. Seaberg Publisher: ISBN: Category : Aerodynamics, Supersonic Languages : en Pages : 36
Book Description
A reevaluation of existing flight data obtained for a supersonic canard missile configuration of the boost-glide type has been made to determine derivatives not previously evaluated. These derivatives, together with those previously evaluated and published, have been utilized to determine some typical airframe frequency responses based on the three-degree-of-freedom longitudinal equations of motion.
Author: Ernest C. Seaberg Publisher: ISBN: Category : Languages : en Pages : 29
Book Description
A reevaluation of existing flight data obtained for a supersonic canard missile configuration of the boost-glide type has been made to determine derivatives not previously evaluated. These derivatives, together with those previously evaluated and published, have been utilized to determine some typical airframe frequency responses based on the three-degree-of-freedom longitudinal equations of motion.
Author: Ernest C. Seaberg
Author: Ernest C. Seaberg
Author: Ernest C. Seaberg
Author: United States. National Advisory Committee for Aeronautics
Author: 
Author: United States. National Advisory Committee for Aeronautics
Author: 
Author: United States. National Advisory Committee for Aeronautics
Author: Defense Documentation Center (U.S.)
Author: 
Author: United States. National Advisory Committee for Aeronautics