Research on Unconventional Layouts of Aircraft

Article Preview

Abstract:

This chapter describes how the overall configuration of the aircraft is decided from the many options available to the designers. From a brief historical perspective the chapter then looks at the unconventional layouts that have been considered in the recent past. Although these have not yet found favor with designers it is worth keeping them in mind as conditions and constraints may change in the future. Such changes could make current layouts less attractive or even not feasible. New designers should start a new project with a completely open mind and this means a careful consideration of all configurations particularly in a historical context.

You might also be interested in these eBooks

Info:

Periodical:

Advanced Materials Research (Volumes 785-786)

Pages:

1189-1192

Citation:

Online since:

September 2013

Authors:

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2013 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] Wolkovitch J. The Joined Wing: An Overview[J]. Journal of Aircraft, I986(5): 161-178.

Google Scholar

[2] Samuels M F. Structural Weight Comparison of a Joined Wing and a Conventional Wing[J]. Journal of Aircraft, 1982, 19(6): 485-491.

DOI: 10.2514/3.57418

Google Scholar

[3] Miura H, Shyu S, Wolkovitch J. Parametric Weight Evaluation of Joined Wings by Structural Optimization[R]. AIAA Paper, March (1985).

DOI: 10.2514/3.45714

Google Scholar

[4] Rhod M D, Selbery B P. Benefits of Duel Wings over Single Wing for High-Performance Business Airplanes[J]. Aircraft, 1984, 21(2): 116-127.

DOI: 10.2514/3.48234

Google Scholar

[5] Stumptl S C, Whitmoyer R A. Horizontal Canards for Two-axis CCV Fighter Control[R]. AGARD-CP-157, (1975).

Google Scholar

[6] Kohlmann D L. Direct Side Force Control for Light Airpllanes[R]. AIAA Paper Nr. 74-862, (1974).

Google Scholar

[7] HUNTER C A, VIKEN S A. Advanced aerodynamic design of passive porosity control effectors. AIAA 2001-0249.

DOI: 10.2514/6.2001-249

Google Scholar