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 ISBNConference contribution with ISSN or ISBN

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 languageEnglish
Title of host publicationProceedings of the 4th CEAS Conference in Linkoping, 2013
Pages7-16
Number of pages10
Publication statusPublished - 2013
Event4th CEAS conference, CEAS2013: "Innovative Europe", Air & Space Conference
- Linköping, Sweden
Duration: 16 Sep 201319 Sep 2013

Conference

Conference4th CEAS conference, CEAS2013: "Innovative Europe", Air & Space Conference
CountrySweden
CityLinköping
Period16/09/1319/09/13

Keywords

  • CFD
  • Applied Aerodynamics
  • Wind Tunnel Test
  • Strake

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