Study on the influence of deflected strake on the rocket plane aerodynamic characteristics

Agnieszka Kwiek; Marcin Figat

Study on the influence of deflected strake on the rocket plane aerodynamic characteristics

Agnieszka Kwiek, Marcin Figat

Research output: Chapter in Book/Conference proceeding with ISSN or ISBN › Conference contribution with ISSN or ISBN › peer-review

Abstract

The paper presents the research on the influence of the movable strake on the basic aerodynamic characteristics of aircraft in tailless configuration. Concept of the movable strake includes deflection of the whole strake (Hinged Strake) and conception of the strake forward flap (SFF) which is attached to leading edge of the strake. The shape of flap and its deflection are considered. The research includes two method of investigation: numerical and experimental.

Original language	English
Title of host publication	Proceedings of the 4th CEAS Conference in Linkoping, 2013
Publisher	Linkoping University Electronic Press
Pages	7-16
Number of pages	10
ISBN (Print)	9789175195193, 9789175195209
Publication status	Published - 2013
Event	4^th CEAS conference, CEAS2013: "Innovative Europe", Air & Space Conference - Linköping, Sweden Duration: 16 Sept 2013 → 19 Sept 2013

Conference

Conference	4^th CEAS conference, CEAS2013: "Innovative Europe", Air & Space Conference
Country/Territory	Sweden
City	Linköping
Period	16/09/13 → 19/09/13

Keywords

CFD
Applied Aerodynamics
Wind Tunnel Test
Strake

Access to Document

http://liu.diva-portal.org/smash/get/diva2:657370/FULLTEXT01.pdf

Cite this

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title = "Study on the influence of deflected strake on the rocket plane aerodynamic characteristics",

abstract = "The paper presents the research on the influence of the movable strake on the basic aerodynamic characteristics of aircraft in tailless configuration. Concept of the movable strake includes deflection of the whole strake (Hinged Strake) and conception of the strake forward flap (SFF) which is attached to leading edge of the strake. The shape of flap and its deflection are considered. The research includes two method of investigation: numerical and experimental.",

keywords = "CFD, Applied Aerodynamics, Wind Tunnel Test, Strake",

author = "Agnieszka Kwiek and Marcin Figat",

year = "2013",

language = "English",

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pages = "7--16",

booktitle = "Proceedings of the 4th CEAS Conference in Linkoping, 2013",

publisher = "Linkoping University Electronic Press",

note = "4th CEAS conference, CEAS2013: {"}Innovative Europe{"}, Air & Space Conference ; Conference date: 16-09-2013 Through 19-09-2013",

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Kwiek, A & Figat, M 2013, Study on the influence of deflected strake on the rocket plane aerodynamic characteristics. in Proceedings of the 4th CEAS Conference in Linkoping, 2013., 10, Linkoping University Electronic Press, pp. 7-16, 4^th CEAS conference, CEAS2013: "Innovative Europe", Air & Space Conference
, Linköping, Sweden, 16/09/13. <http://liu.diva-portal.org/smash/get/diva2:657370/FULLTEXT01.pdf>

Study on the influence of deflected strake on the rocket plane aerodynamic characteristics. / Kwiek, Agnieszka; Figat, Marcin.
Proceedings of the 4th CEAS Conference in Linkoping, 2013. Linkoping University Electronic Press, 2013. p. 7-16 10.

Research output: Chapter in Book/Conference proceeding with ISSN or ISBN › Conference contribution with ISSN or ISBN › peer-review

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AU - Kwiek, Agnieszka

AU - Figat, Marcin

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N2 - The paper presents the research on the influence of the movable strake on the basic aerodynamic characteristics of aircraft in tailless configuration. Concept of the movable strake includes deflection of the whole strake (Hinged Strake) and conception of the strake forward flap (SFF) which is attached to leading edge of the strake. The shape of flap and its deflection are considered. The research includes two method of investigation: numerical and experimental.

AB - The paper presents the research on the influence of the movable strake on the basic aerodynamic characteristics of aircraft in tailless configuration. Concept of the movable strake includes deflection of the whole strake (Hinged Strake) and conception of the strake forward flap (SFF) which is attached to leading edge of the strake. The shape of flap and its deflection are considered. The research includes two method of investigation: numerical and experimental.

KW - CFD

KW - Applied Aerodynamics

KW - Wind Tunnel Test

KW - Strake

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M3 - Conference contribution with ISSN or ISBN

SN - 9789175195193

SN - 9789175195209

SP - 7

EP - 16

BT - Proceedings of the 4th CEAS Conference in Linkoping, 2013

PB - Linkoping University Electronic Press

T2 - 4th CEAS conference, CEAS2013: "Innovative Europe", Air & Space Conference

Y2 - 16 September 2013 through 19 September 2013

ER -

Study on the influence of deflected strake on the rocket plane aerodynamic characteristics

Abstract

Conference

Keywords

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