Method and system for gathering pressure signature data...

Measuring and testing – Wind tunnel: aerodynamic wing and propeller study

Reexamination Certificate

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C073S170020

Reexamination Certificate

active

11425909

ABSTRACT:
Disclosed is a method of and system for gathering off-body pressure signature data from a scaled model in a wind tunnel. The data is gathered using a probe having multiple longitudinally disposed static pressure ports. Because of the number of ports and their spacing, the probe is able to remain stationary in the tunnel for the entire range of Mach numbers and model positions to be tested. Thus, tunnel flow characteristics can be easily and effectively removed. The system also has an automated model positioning system which enables settings at different pitch, yaw, and roll angles. This enables the user to locate the model so that it can be traversed at a fixed distance above the probe while maintaining the desired angular orientation of the model. By repeatedly traversing the model at different angular orientations, a detailed and accurate off-body pressure distribution can be obtained. The wind tunnel test technique captures full off-body pressure signatures in a complete 360 degree azimuthal range.

REFERENCES:
patent: 6698684 (2004-03-01), Henne et al.
patent: 6729577 (2004-05-01), Morgenstern
patent: 6824092 (2004-11-01), Franklin, III et al.
patent: 6854687 (2005-02-01), Morgenstern et al.
patent: 6921045 (2005-07-01), Chang et al.
patent: 6942178 (2005-09-01), Morgenstern et al.
patent: 2005/0045764 (2005-03-01), Morgenstern et al.
patent: 2005/0067525 (2005-03-01), Morgenstern et al.
George, A.R., “Lower Bounds For Sonic Booms In the Midfield,” AIAA Journal, vol. 7, No. 8, pp. 1542-1545, Aug. 1969.
George, A.R. and Seebass, R., “Sonic Boom Minimization Including Both Front and Rear Shocks,” AIAA Journal, vol. 9, No. 10, pp. 2091-2093, Oct. 1971.
Graham, David H; Dahlin, John A.; Meredith, Keith B.; and Vadnais, Jay L., “Aerodynamic Design Of shaped Sonic Boom Demonstration Aircraft,” 43rd AIAA Aerospace Sciences Meeting And Exhibit, pp. 1-7, Jan. 10-13, 2005.
Henne, Preston A., “Small Supersonic Civil Aircraft,” Presentation at Aircraft Noise And Emissions Reduction Symposium, May 24-26, 2005.
Lyman, Victor and Morgenstern, John M., “Calculated And Measured Pressure Fields For An Aircraft Designed For Sonic-Boom Alleviation,”, 22nd Applied Aeronautics Conference, pp. 1-7, Aug. 16-19, 2004.
Mack, Robert J. and Needleman, Kathy E., “a Methodology For Designed Aircraft To Low Sonic Boom Constraints,” NASA Technical Memorandum 4246, pp. 1-23, 1991.
Mohammadi, Bijam, “Optimization Of Aerodynamic And Acoustic Performance Of Supersonic Civil Transports,” pp. 285-296, Center For Turbulance Research Proceedings of the Summer Program 2002.
Mohammadi, Bijan, and Pironneau, Olivier, “Shape Optimization In Fluid Mechanics,” Annu. Rev. Fluid Mech., pp. 255-279, 2004.
Morgenstern, John M., “Wind Tunnel Testing of a Sonic Boom Minimized Tail-Braced Wing Transport Configuration,” AIAA 2004-4536, 2004.
Plotkin, Kenneth J., Sonic Boom: Origins, Modeling And Effects, Wyle Laboratories, pp. 1-43, Jun. 8-9, 2004.
Pawlowski, Joseph W.; Graham, David H., and Boccadoro, Charles H., “Origins And Overview Of The Shaped Sonic Boom Demonstration Program,” 43rd AIAA Aerospace Sciences Meeting And Exhibit, pp. 1-14, Jan. 10-13, 2005.
Seebass, A.R. and George, A.R., “Design And Operation Of Aircraft To Minimize Their Sonic Boom,” J. Aircraft, vol. 11, No. 9, pp. 509-517, Sep. 1974.
Seebass, Richard and Argrow, Brian, Sonic Boom Minimization Revisited, American Insititue Of Aeronautics And Astronautics, Inc., AIAA-98-2956, pp. 1 14, 1998.
Tam, Tim; Ruffin, Stephen; Gage, Peter; Yates, Leslie; and Morgenstern, John Sonic Boom Testing Of Artificially Blunted Leading Edge (Able) Concepts In The NASA AMES Aeroballistic Range, pp. 1-13, AIAA 2000-1011, 2000.
Whitham, “Sonic Booms,” Extensions of the Theroy, Section 9.3, p. 337, 1974.
Vazquez, Mariano and Dervieux, Alain, “Sonic Boom Optimization Of A Supersonic Business Jet,” 2002-2003.

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