LEX and wing tip plates’ interaction on the Rocket Plane in tailless configuration-Reference-Cited by-同舟云学术

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

Published:2016-02 Issue:1224 Volume:120 Page:255-270
ISSN:0001-9240
Container-title:The Aeronautical Journal
language:en
Short-container-title:Aeronaut.j.

Author:

Kwiek A.,Figat M.

Abstract

ABSTRACTThe 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.

Publisher

Cambridge University Press (CUP)

Subject

Aerospace Engineering

Reference15 articles.

1. 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.

2. 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].

3. 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.

4. 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].

Cited by 9 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. Study of the Impact of Aerodynamic Model Fidelity on the Flight Characteristics of Unconventional Aircraft;Applied Sciences;2023-11-20

2. Experimental study of the effect of the LEX angle on the flow pattern of a diamond wing with an airfoil cross section;Journal of Visualization;2023-08-31

3. The Study of Selected Aspects of the Suborbital Vehicle Return Flight Trajectory;Aerospace;2023-05-22

4. An investigation into directional characteristics of the rocket plane in a tailless configuration;CEAS Space Journal;2022-08-29

5. Results of simulation and scaled flight tests performed on a rocket-plane at high angles of attack;Aircraft Engineering and Aerospace Technology;2021-04-05