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ISSN Печать: 1948-2590
ISSN Онлайн: 1948-2604
MOTION CHARACTERISTICS FOR A BLUNTED CYLINDER WITH STABILIZERS ACCORDING TO THE RESULTS OF AEROBALLISTIC EXPERIMENT
Краткое описание
The methodology and the testing results on investigation of the effect of the stabilizers located in the aft part of aircraft as a function of the parameters of the aircraft motion and their aerodynamic characteristics are presented. The paper describes the experiments in an aeroballistic dash as well as the methodology of optical registration of flight parameters and shadow spectra of the flow around the model of a blunted cylinder with stabilizers and the results obtained.
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