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Cal Poly's AMELIA 10 Foot Span Hybrid Wing-Body Low Noise CESTOL Aircraft Wing Tunnel Test and Experimental Results Overview
51st AIAA Aerospace Sciences Meeting Proceedings: Grapevine, TX
  • Kristina K. Jameson, California Polytechnic State University - San Luis Obispo
  • David D. Marshall, California Polytechnic State University - San Luis Obispo
  • Robert Ehrmann, California Polytechnic State University - San Luis Obispo
  • Jonathon A. Lichtwardt, California Polytechnic State University - San Luis Obispo
  • Eric N. Paciano, California Polytechnic State University - San Luis Obispo
  • Robert J. Englar, Georgia Institute of Technology - Main Campus
  • William C. Hornes, NASA Ames Research Center
Publication Date
1-7-2013
Abstract

A collaboration between California Polytechnic Corporation with Georgia Tech Research Institute (GTRI) and DHC Engineering worked on a NASA NRA to develop predictive capabilities for the design and performance of Cruise Efficient, Short Take-Off and Landing (CESTOL) subsonic aircraft. The work presented in this paper gives details of a large scale wind tunnel effort to validate predictive capabilities for this NRA for aerodynamic and acoustic performance during takeoff and landing. The model, Advanced Model for Extreme Lift and Improved Aeroacoustics {AMELIA), was designed as a 100 passenger, N+2 generation, regional, cruise efficient short takeoff and land (CESTOL) airliner with hybrid blended wing-body with circulation control. AMELIA is a 1/11 scale with a corresponding 10ft wing span. The National Full-Scale Aerodynamic Complex (NFAC) 40ft by 80ft wind tunnel was chosen to perform the large-scale wind tunnel test. The NFAC was chosen because both aerodynamic and acoustic measurements will be obtained simultaneously, the tunnel is large enough that the downwash created by the powered lift did not impinge on the tunnel walls, and the schedule and cost fit into Cal Poly's time frame and budget. Several experimental measurement techniques were used to obtain the necessary data to validate predictive codes being developed as apart of this effort: along with the traditional forces and moments measurements, stationary microphones were used to obtain far-field acoustic measurements including a 48 element phased array, the Fringe-Image Skin Friction (FISF) technique was used to measure the global skin friction on the wing, surface mounted steady and unsteady pressure transducers were used to obtain local pressure distributions over the model, and oil and smoke flow visualization techniques were employed to understand the effects of the powered lift system in AMELIA. The paper gives a brief summary of AMELIA's performance for variable tunnel speed, momentum mass flow, engine simulator height, and angle of attack.

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Citation Information
Kristina K. Jameson, David D. Marshall, Robert Ehrmann, Jonathon A. Lichtwardt, et al.. "Cal Poly's AMELIA 10 Foot Span Hybrid Wing-Body Low Noise CESTOL Aircraft Wing Tunnel Test and Experimental Results Overview" 51st AIAA Aerospace Sciences Meeting Proceedings: Grapevine, TX (2013)
Available at: http://works.bepress.com/ddmarsha/35/