Computational Solution of Aircraft Stability Derivatives
نویسندگان
چکیده
منابع مشابه
Applications of Computational Methods for Dynamic Stability and Control Derivatives
Initial steps in the application of a low-order panel method computational fluid dynamics (CFD) code to the calculation of aircraft dynamic stability and control (S&C) derivatives are documented. Several capabilities, unique to CFD but not unique to this particular demonstration, are identified and demonstrated in this paper. These unique capabilities complement conventional S&C techniques and ...
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Initial steps in the application of a low-order ............. ,.,.1 ....... , ................ r1 ,........,.TY\.."l1t .... t;",., .... l fll11rl rl"n':UTI1 .. c (r~n\ pU.I"". 111,",l'I\.J~ ............ 11.1-''-&'""'".\. ..... ". II\"&.~ -,J .I"IIII~U \ _ .. A..-I code to the calculation of aircraft dynamic stability and control (S&C) derivatives are documented. Several capabilities, unique to ...
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ژورنال
عنوان ژورنال: International Conference on Aerospace Sciences and Aviation Technology
سال: 1997
ISSN: 2636-364X
DOI: 10.21608/asat.1997.25388