Application of three-dimensional aerodynamics for calculating trim parameters and flight loads in MSC.Nastran


Cite item

Full Text

Open Access Open Access
Restricted Access Access granted
Restricted Access Subscription Access

Abstract

The paper deals with solving the problem on calculating the flight loads using a three-dimensional aerodynamic model. An algorithm and an example of calculation are presented.

About the authors

M. V. Kvyatkovskaya

PAO Tupolev

Email: regina.leontjeva@gmail.com
Russian Federation, naberezhnaya Akademika Tupoleva 17, Moscow, 105005

R. V. Leont’eva

PAO Tupolev

Author for correspondence.
Email: regina.leontjeva@gmail.com
Russian Federation, naberezhnaya Akademika Tupoleva 17, Moscow, 105005


Copyright (c) 2017 Allerton Press, Inc.

This website uses cookies

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

About Cookies