Analysis of the structure of the third variation of roll moment coefficient during hypersonic flow about bodies of revolution with small spatial surface variations on the basis of differential locality hypothesis method

Cover Page

Cite item

Full Text

Abstract

The paper deals with the problem of evaluating the constituents of the third order of roll moment smallness during supersonic flow at small angles of attack of bodies close to bodies of revolution. An expression is derived on the basis of the method of differential locality hypothesis, and the structure of the third variation of roll moment coefficient is analysed, its complete composition is defined. Integral expressions of seven constituents of the third variation are obtained, physical interpretation of each is given.

About the authors

V. A. Danilkin

Joint-Stock Company “State Rocket Centre named after academician V. P. Makeyev”, Miass

Author for correspondence.
Email: src@makeyev.ru
Russian Federation

G. F. Kostin

Joint-Stock Company “State Rocket Centre named after academician V. P. Makeyev”, Miass

Email: src@makeyev.ru
Russian Federation

Yu. A. Mokin

Joint-Stock Company “State Rocket Centre named after academician V. P. Makeyev”, Miass

Email: src@makeyev.ru
Russian Federation

N. N. Tikhonov

Joint-Stock Company “State Rocket Centre named after academician V. P. Makeyev”, Miass

Email: src@makeyev.ru
Russian Federation

References

Supplementary files

Supplementary Files
Action
1. JATS XML

Copyright (c) 2015 VESTNIK of the Samara State Aerospace University

This website uses cookies

You consent to our cookies if you continue to use our website.

About Cookies