An Integrated Preliminary Approach Elaboration for the Analysis of a Blended Wing Body Aerostructure Concept-Reference-Cited by-同舟云学术

An Integrated Preliminary Approach Elaboration for the Analysis of a Blended Wing Body Aerostructure Concept

Published:2023 Issue: Volume: Page:331-340
ISSN:2195-4356
Container-title:Lecture Notes in Mechanical Engineering
language:
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Author:

Hakim Mohamed,Choukri Saad

Publisher

Springer International Publishing

Link

https://link.springer.com/content/pdf/10.1007/978-3-031-23615-0_34

Reference23 articles.

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3. Dussart, G., et al.: Flight dynamic modelling and simulation of large flexible aircraft. Flight Physics-Models, Techniques and Technologies, pp. 49–72 (2018)

4. Williams, J.E., Vukelich, S.R.: The USAF stability and control digital DATCOM, vol. II. Implementation of DATCOM Methods. Technical report, Mcdonnell Douglas Astronautics Co St Louis Mo (1979)

5. Hess, J.L., Smith, A.M.O.: Calculation of nonlifting potential flow about arbitrary three-dimensional bodies. J. Ship Res. 8(04), 22–44 (1964)

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