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Performance Enhancement of a Full-Scale Vertical Tail Model Equipped with Active Flow Control

Whalen, Edward A. and Lacy, Douglas and Lin, John C. and Andino, Marlyn Y. and Washburn, Anthony E. and Graff, Emilio and Wygnanski, Israel J. (2015) Performance Enhancement of a Full-Scale Vertical Tail Model Equipped with Active Flow Control. In: 53rd AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics , Reston, VA, Art. No. 2015-0784. ISBN 978-1-62410-343-8. https://resolver.caltech.edu/CaltechAUTHORS:20191017-075901660

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Abstract

This paper describes wind tunnel test results from a joint NASA/Boeing research effort to advance active flow control (AFC) technology to enhance aerodynamic efficiency. A full-scale Boeing 757 vertical tall model equipped with sweeping jet actuators was tested at the National Full-Scale Aerodynamics Complex (NIFAC) 40- by 80-Foot Wind Tunnel (40x80) at NASA Ames Research Center. The model was tested at a nominal airspeed of 100 knots and across rudder deflections and sideslip angles that covered the vertical tail flight envelope. A successful demonstration or AFC-enhanced vertical tail technology was achieved. A 31-actuator configuration significantly increased side force (by greater than 20%) at a maximum rudder deflection of 30°. The successful demonstration of this application has cleared the way for a flight demonstration on the Boeing 757 ecoDemonstrator in 2015.


Item Type:Book Section
Related URLs:
URLURL TypeDescription
https://doi.org/10.2514/6.2015-0784DOIArticle
https://ntrs.nasa.gov/search.jsp?R=20150006853OrganizationNASA Technical Reports Server
ORCID:
AuthorORCID
Lin, John C.0000-0003-2794-184X
Additional Information:© 2015 American Institute of Aeronautics and Astronautics. Published Online: 3 Jan 2015. This multi-organizational and multidisciplinary teaming effort involved many people who provided valuable contributions through their detailed work and/or expert guidance. The contributors have come from within the NASA/Boeing team and their partners. The NASA/Boeing collaboration was executed through a Space Act Agreement (Annex 8 to SAA1-1155). The NASA ERA project sponsored the sweeping jet AFC technology via Caltech (TEAMS 2 Contract NNL12AA09C) and the University of Arizona (direct subcontract). The ERA project also sponsored the wind tunnel test at NFAC (NIPR# NNL12AA13T). The authors would like to thank key personnel in the following organizations for their excellent support during the course of this investigation: Boeing Commercial Airplanes: Kate Nowicki (technology manager), John Brandt (stability & control), Kyle Ford (loads & dynamics), and Helen Mooney (aerodynamics).
Group:GALCIT
Funders:
Funding AgencyGrant Number
NASANNL12AA09C
University of ArizonaUNSPECIFIED
NASANNL12AA13T
Other Numbering System:
Other Numbering System NameOther Numbering System ID
AIAA Paper2015-0784
Record Number:CaltechAUTHORS:20191017-075901660
Persistent URL:https://resolver.caltech.edu/CaltechAUTHORS:20191017-075901660
Official Citation:Performance Enhancement of a Full-Scale Vertical Tail Model Equipped with Active Flow Control. Edward A. Whalen, Doug S. Lacy, John C. Lin, Marlyn Y. Andino, Anthony E. Washburn, Emilio C. Graff, and Israel J. Wygnanski. 53rd AIAA Aerospace Sciences Meeting. January 2015. https://doi.org/10.2514/6.2015-0784
Usage Policy:No commercial reproduction, distribution, display or performance rights in this work are provided.
ID Code:99319
Collection:CaltechAUTHORS
Deposited By: Tony Diaz
Deposited On:22 Oct 2019 22:33
Last Modified:23 Oct 2019 15:05

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