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TsAGI Science Journal

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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

Том 51, Выпуск 4, 2020, pp. 355-363
DOI: 10.1615/TsAGISciJ.2020037245
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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.

ЛИТЕРАТУРА
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