Hostname: page-component-cd9895bd7-gbm5v Total loading time: 0 Render date: 2024-12-22T11:36:43.864Z Has data issue: false hasContentIssue false
  • English
  • Français

LEX and wing tip plates’ interaction on the Rocket Plane in tailless configuration

Published online by Cambridge University Press:  29 February 2016

A. Kwiek  and
M. Figat
A. Kwiek*
Affiliation:
The Institute of Aeronautics and Applied Mechanics, Aircraft Design Department, Warsaw University of Technology, WarsawPoland
M. Figat*
Affiliation:
The Institute of Aeronautics and Applied Mechanics, Aircraft Design Department, Warsaw University of Technology, WarsawPoland
*
[email protected]
[email protected]
Get access Rights & Permissions [Opens in a new window]

Abstract

The article includes study on the influence of a LEX (leading-edge extension) and wing tip plates on aerodynamic characteristics of the Rocket Plane in tailless configuration for manned suborbital flights. The research was conducted only for the low speed regime in the wind tunnel at the Warsaw University of Technology. Tests were carried out for a few configurations of the Rocket Plane. Moreover, two shapes of LEX were investigated. Analysis of results was focused on the aerodynamic synergism effect only. The influence of LEX and the wing tip plates of the Rocket Plane on the aerodynamic coefficients was identified.

Keywords

Aerodynamicswind tunnel testtailless aircraftLEXaerodynamicsaircraft designspace
Type
Research Article
Information
The Aeronautical Journal , Volume 120 , Issue 1224 , February 2016 , pp. 255 - 270
Copyright
Copyright © Royal Aeronautical Society 2016 

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

REFERENCES

1.Galiński, C., Goetzendorf-Grabowski, T., Mieszalski, D. and Stefanek, Ł.A concept of two-staged spaceplane for suborbital tourism, Trans Inst Aviation, 2007, 191, (47), pp 33–42.Google Scholar
2.Figat, M., Galiński, C. and Kwiek, A. Modular Aeroplane System. A Concept and Initial Investigation, Proceeding of the 28th International Congress of the Aeronautical Sciences 2012, Brisbane Australia, paper number ICAS 2012-1.3.2.Google Scholar
3.Luckring, J.M.Aerodynamic of strake-wing interactions, J Aircraft, 1979, 16, (11), pp 756–762.CrossRefGoogle Scholar
4.Polhamus, E.C. A Concept of the vortex lift of sharp-edge delta wing based on a leading-edge-suction analogy, NASA technical note NASA TN D-3767, 1966, Washington, DC, US.Google Scholar
5.Lamar, J. Analysis and design of strake-wing configuration, J Aircraft, 1980, 17, (1), pp 20–27.CrossRefGoogle Scholar
6.Goodall, J. and Miller, J.Lockheed's SR-71 ‘Blackbird’ Family A-12, F-12, M-21, D-21, SR-71, 2002, Ian Allan Publishing.Google Scholar
7.Figat, M., Kwiek, A. and Seneńko, K. Aerodynamic Design of the Strake for the Rocket Plane in Tailless Configuration, Proceeding of the 29 International Congress of the Aeronautical Sciences 2014, St. Petersburg Russia, paper number ICAS 2014_0751.Google Scholar
8.Witoszyński, C. Travaux de L'Institut Aerodynamique de Varsovie. Fascicule V, Warszawa 1932, http://bcpw.bg.pw.edu.pl/dlibra/docmetadata?id=3157&from=&dirids=1&ver_id=49254&lp=4&QI=!EFCF9417B69770894E5914376646D2BD-59 a document in Polish and French [cited 20 April 2015].Google Scholar
9.Grobelny, M. Badanie i modernizacja tunelu aerodynamicznego, Master Thesis, in Polish (Research and improvement of the wind tunnel), not published, 2013.Google Scholar
10.Lamar, J.E. and Frink, N.T. Experimental and Analytical Study of the Longitudinal Aerodynamic Characteristics of Analytically and Empirically Designed Strake-Wing Configurations at Subcritical Speeds, NASA Technical Paper 1803, 1981, Virginia, Hampton, US.CrossRefGoogle Scholar
11.Jaracz, P. and Szefliński, Z. Elementarz rachunku błędu pomiarowego, Faculty of Physics, University of Warsaw, available at: http://msos.igf.fuw.edu.pl/msos/elem%20rach%20bledu.pdf [cited 20 April 2015].Google Scholar
12.Zhao, W., Kwak, D. and Rinoie, K. Studies on Improvement of nonlinear Pitching Moment Characteristics of Cranked-Arrow Wing proceeding of the 28th International Congress of the Aeronautical Sciences 2012, Brisbane Australia, paper number ICAS 2012–3.2.1.Google Scholar
13.Anderson, J.D. Jr.Fundamentals of Aerodynamics, 3rd ed, 2001, Published by McGraw-Hill, New York, US.Google Scholar
14.Bertin, J. J.Aerodynamics for Engineers, 4th ed, 2002, Published by Prentice Hall, Upper Saddle River, NJ, US.Google Scholar
15.Gursul, I., Gordnier, R. and Visbal, M. Unsteady aerodynamics of nonslender delta wings, Prog Aerospace Sci, 2005, 41, pp 515–557.CrossRefGoogle Scholar