An Alternate Configuration for a Regional Transport Airplane.-Reference-Cited by-同舟云学术

An Alternate Configuration for a Regional Transport Airplane.

Published:2002 Issue:148 Volume:45 Page:94-101
ISSN:0549-3811
Container-title:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:en
Short-container-title:Trans. Japan Soc. Aero. S Sci.

Author:

Pambagjo Tjoetjoek Eko,Nakahashi Kazuhiro,Matsushima Kisa

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://www.jstage.jst.go.jp/article/tjsass/45/148/45_148_94/_pdf

Reference14 articles.

1. 1) Wood, R. M. and Bauer, S. X. S.: Flying Wings/Flying Fuselage, AIAA Paper 2001-0311, 2001.

2. 2) Liebeck, R. H., Page, M. A. and Rawdon, B. K.: Blended Wing Body Subsonic Commercial Transport, AIAA Paper 98-0438, 1998.

3. 3) Smith, H.: College of Aeronautics Blended Wing Body Development Programme, Proc. of ICAS 2000, ICAS2000-1.1.4, 2000.

4. 4) Bolsunovsky, A. L., Buzoverya, N. P., Gurevich, B. I., Denisov, V. E., Shkadov, L. M. and Udzhukhu, A. Y.: Investigations on Possible Characteristic of FW Superhigh Seating Capacity Airplane, Proc. of ICAS 2000, ICAS2000-1.1, 2000.

5. 5) Martinez-Val, R. and Schoep, E.: Flying Wing Versus Conventional Transport Airplane: The 300 Seat Case, Proc. of ICAS 2000, 2000.

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Preliminary Aerodynamic Shape Optimization of a Blended-Wing-Body Aircraft Configuration;49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2011-01-04

2. Current Capability of Unstructured-Grid CFD and a Consideration for the Next Step;High Performance Computing on Vector Systems 2007