Aerodynamic compatibility of an aircraft and loads

Aviation technics and technology


Аuthors

Smirnov V. U.

Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

Abstract

The analysis of an aerodynamic interference in "an aircraft - bulky load" system is conducted. The main theses of the concept of aerodynamic compatibility are formulated. The value of researches of aerodynamic compatibility in the system functioning quality researches in "an aircraft - bulky load" system is shown.


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