Abstract The mathematical models (MM) of aircraft aerodynamic loads in terms of aerodynamic derivatives are reviewed. It was shown that the novel MM including an ordinary linear differential first-order equation makes it possible not only to describe the unsteady effects at the near-critical angles of attack more adequately but to solve the problem of dividing the aerodynamic derivative systems for a wide class of load-carrying systems with a sufficient accuracy.
On the issue of dividing the aerodynamic derivative systems for the aircraft flight dynamics problems
Russian Aeronautics (Iz VUZ) ; 54 , 3 ; 298-302
2011-09-01
5 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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