Physics and control of the flow over a generic trapezoidal wing planform

Sebastian Endrikat, Bernhard Roentsch, Jesse Little, Lutz Taubert, Israel Wygnanski, Charles Farbos de Luzan, Ephraim Gutmark

Research output: Chapter in Book/Report/Conference proceedingConference contribution

2 Scopus citations

Abstract

This work provides discussion of key geometric features that influence the aerodynamic performance of trapezoidal wings. Subject of the survey is a highly tapered wing model with low aspect ratio, based on a NACA0012 airfoil section. A comparison to a non-tapered swept-back wing demonstrates advantageous stability properties that motivate this work. Experimentally obtained force and moment data, surface flow visualization and PIV are presented along with computational results. It is found that the strength and formation of the leading-edge vortex can be altered by modifying the nose radius or droop of the model. Implications of those changes on integral aerodynamic properties are evaluated. A triangular and a parallel flap geometry that exhibit fundamentally different flow conditions are discussed. Focus is placed on the latter to account for non-aerodynamic requirements of typical military aircraft. The capability of sweeping jet actuators to redirect or attach flow is assessed to examine the resulting effects on forces and moments. Additionally, the possibility of applying active flow control as a means to maneuver is explored.

Original languageEnglish (US)
Title of host publication54th AIAA Aerospace Sciences Meeting
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624103933
DOIs
StatePublished - 2016
Event54th AIAA Aerospace Sciences Meeting, 2016 - San Diego, United States
Duration: Jan 4 2016Jan 8 2016

Publication series

Name54th AIAA Aerospace Sciences Meeting
Volume0

Other

Other54th AIAA Aerospace Sciences Meeting, 2016
CountryUnited States
CitySan Diego
Period1/4/161/8/16

ASJC Scopus subject areas

  • Aerospace Engineering

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