Preliminary Assessment of the Weight of the Aircraft Fuselage as a Result of the Transition to Composite Materials-Reference-Cited by-同舟云学术

Preliminary Assessment of the Weight of the Aircraft Fuselage as a Result of the Transition to Composite Materials

Published:2020-09 Issue:3 Volume:63 Page:386-396
ISSN:1068-7998
Container-title:Russian Aeronautics
language:en
Short-container-title:Russ. Aeronaut.

Author:

Kretov A. S.,Shataev P. A.

Publisher

Allerton Press

Subject

Aerospace Engineering

Link

http://link.springer.com/content/pdf/10.3103/S1068799820030034.pdf

Reference23 articles.

1. Bolkhovitinov, V.F., Puti razvitiya letatel’nykh apparatov (Ways of Development of Aircraft), Moscow: Oborongiz, 1962.

2. Mishin, V.F., Liseitsev, N.K., et al., Proektirovanie samoletov (Design of Aircraft), Eger, S.M. (Ed.), Moscow: Mashinostroenie, 1983.

3. Korol’kov, O.N., The Equation and the Region of the Airplane Existence, Polet, 2001, no. 10, pp. 45–52.

4. Proektirovanie samoletov (Design of Aircraft), Pogosyan, M.A., Ed., Moscow: Innovatsionnoe Mashinostroenie, 2018, 864 p.

5. Sheinin, V.M., Vesovaya i transportnaya effektivnost’ passazhirskikh samoletov (Weight and Transport Efficiency of Passenger Aircraft), Moscow: Oborongiz, 1962, 363 p.

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