Continuing evolution of aerodynamic concept development using collaborative numerical and experimental evaluations

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering

Volumn 220, Issue 6, 2006, Pages 545-557

  Cummings, R M ^a   Morton, S A ^a  

^a UNITED STATES AIR FORCE ACADEMY   (United States)

Author keywords

Computational fluid dynamics; Experimental aerodynamics; Unsteady aerodynamics

Indexed keywords

CLOSED LOOP CONTROL SYSTEMS; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SUPPORTED COOPERATIVE WORK; FLOW CONTROL; PROJECT MANAGEMENT; UNMANNED VEHICLES;

AERODYNAMIC CONTROL; EXPERIMENTAL AERODYNAMICS; UNMANNED COMBAT AIR VEHICLE; UNSTEADY AERODYNAMICS;

AERODYNAMICS;

EID: 33947588350     PISSN: 09544100     EISSN: None     Source Type: Journal    
DOI: 10.1243/09544100JAERO71     Document Type: Article

References (14)

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3. Cummings, R. M., Morton, S. A., and Siegel, S. G. Computational simulation and experimental measurements for a delta wing with periodic suction and blowing. J. Airc., 2003, 40(5), 923-931.
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11. Cummings, R. M., Divine, J. A., Yechout, T., Wetlesen, D., and Kealos, J. Numerical evaluation of the flowfield for a high fineness ratio body with drag brakes. AIAA 44th Aerospace Sciences Meeting, January 2006, AIAA paper 2006-0668 (AIAA, Reston, VA).
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