Zobrazeno 1 - 2
of 2
pro vyhledávání: '"indicial response functional"'
AIAA Atmospheric Flight Mechanics Conference & Exhibit, August 5-8, 2002, Monterey, California, United States
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Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______1674::3aa45ea3836d2089367622ff6cc39084
https://nrc-publications.canada.ca/eng/view/object/?id=8d32b0ce-1acc-40c6-855c-aa72e18cf20e
https://nrc-publications.canada.ca/eng/view/object/?id=8d32b0ce-1acc-40c6-855c-aa72e18cf20e
Autor:
Xing-Zhong Huang
Publikováno v:
21st AIAA Applied Aerodynamics Conference.
A modified nonlinear indicial response method, in conjunction with internal state-space representation (NIRISS) was proposed. It has been found that for a delta wing, its leading-edge vortex has a dominant effect on its aerodynamics and therefore the