Structural weight estimation of a flying wing with a pressurized wing box

• Autorzy: Rodriquez C. , Martinez-Val R. , Gutierrez L.
• Konferencja: Proceedings of the Fourth Seminar on Recent Research and Design Progress in Aeronautical Engineering and its Influence on Education/seminar(IV; 30.11-02.12.2000; Warszawa, Polska)
• Języki publikacji: EN

Abstrakty

EN

The present paper will introduce a prediction method that will allow for estimation of the structural weight of a transport flying with an approximate capacity of 300 passengers. The flying wing payload will be located between the front and rear spars, and up to half the span approximately, which implies that the study of the wing structure will have two different parts; i.e., the external structure that will be of conventional architecture apart from its dimensions that will be bigger and the internal structure, no conventional, where the torsion box will be pressurized and with all the equipment required for passenger and, cargo transportation.

Słowa kluczowe

EN

aircrafts; flying wing; wing box; aircraft design

PL

samoloty; konstrukcja samolotu; skrzydła samolotu

• Wydawca: Institute of Aeronautics and Applied Mechanics, Warsaw University of Technology
• Czasopismo: Research Bulletin / Warsaw University of Technology, Institute of Aeronautics and Applied Mechanics
• Rocznik: 2000
• Tom: nr 10
• Strony: 177--182
• Opis fizyczny: Bibliogr. 9 poz., wykr.

Twórcy

autor

Rodriquez C.

autor

Martinez-Val R.

autor

Gutierrez L.

• Universidad Politecnica de Madrid, (UPM), Madrid, Spain