Analytic Theory of Optimal Plane Change by Low Aerodynamic Forces

1997 ◽  
Vol 45 (3) ◽  
pp. 329-347 ◽  
Author(s):  
Der-Ming Ma ◽  
Chi-Hang Wu ◽  
Nguyen X. Vinh

1990 ◽  
Author(s):  
NGUYEN VINH ◽  
DER-MING MA


Author(s):  
H. P. F. Swinnerton-Dyer




2018 ◽  
Vol 49 (1) ◽  
pp. 43-64
Author(s):  
Mikhail Alekseyevich Golovkin ◽  
Andrey Aleksandrovich Efremov ◽  
Miroslav Sergeevich Makhnev


1981 ◽  
Author(s):  
W. ROWE ◽  
H. CUNNINGHAM
Keyword(s):  


1997 ◽  
Author(s):  
Sang-Young Park ◽  
I. Ross ◽  
I. Ross ◽  
Sang-Young Park


1990 ◽  
Author(s):  
Chih-Ming Ho ◽  
Ismet Gursul ◽  
Chiang Shih ◽  
Hank Lin ◽  
Mario Lee


Author(s):  
Junji Maeda ◽  
Takashi Takeuchi ◽  
Eriko Tomokiyo ◽  
Yukio Tamura

To quantitatively investigate a gusty wind from the viewpoint of aerodynamic forces, a wind tunnel that can control the rise time of a step-function-like gust was devised and utilized. When the non-dimensional rise time, which is calculated using the rise time of the gusty wind, the wind speed, and the size of an object, is less than a certain value, the wind force is greater than under the corresponding steady wind. Therefore, this wind force is called the “overshoot wind force” for objects the size of orbital vehicles in an actual wind observation. The finding of the overshoot wind force requires a condition of the wind speed recording specification and depends on the object size and the gusty wind speed.



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