Optimization Procedure for Design of High‐Speed Prop‐Rotors
Publication: Journal of Aerospace Engineering
Volume 7, Issue 2
Abstract
An optimization procedure has been developed to address the complex and conflicting requirements associated with the design of high‐speed proprotor aircraft. Since the key technical issues are maintenance of propulsive efficiency and aeroelastic stability in high‐speed cruise without deteriorating figure of merit in hover, rotor aerodynamic performance and aeroelastic analysis are coupled, inside a closed loop, to the optimizer. The discipline couplings provide actual blade air‐loads, during hover and cruise, and also provide realistic blade designs. The propulsive efficiency in high‐speed cruise is used as the objective function. Constraints are also imposed on the aeroelastic stability in axial flight and the rotor figure of merit in hover. Both structural and planform design variables are used. The optimization procedure yields significant improvements in the aerodynamic characteristics of the rotor. Off‐design performance studies, conducted with the optimum blade, show overall design improvements.
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References
1.
Barthelemy, J.‐F. M., Coen, P. G., Wrenn, G., Riley, M. F., and Dovi, A. R. (1990). “Application of multidisciplinary optimization methods to the design of a supersonic transport.” Proc., 3rd Air Force/NASA Symp. on Recent Adv. in Multidisciplinary Anal. and Optimization, National Aeronautics and Space Administration, (NASA), Washington D.C.
2.
Benoit, B., and Bousquet, J. M. (1990). “Aerodynamic design of a tilt‐rotor blade.” 17th Congr. of Int. Council of the Aeronautical Sci., Stockholm, Sweden, 1–9.
3.
Celi, R., and Friedmann, P. P. (1987). “Efficient structural optimization of rotor blades with straight and swept tips.” Proc., 13th European Rotorcraft Forum, Arles, France.
4.
Chattopadhyay, A., Walsh, J. L., and Riley, M. F. (1991). “Integrated aerodynamic load/dynamic optimization of helicopter rotor blades.” AIAA J. Aircraft, II, 58–65.
5.
Chattopadhyay, A. (1992). “Vibration reduction in an articulated rotor blade using structural optimization.” Engrg. Optimization, 19, 37–50.
6.
Chattopadhyay, A., and Chiu, Y. D. (1992). “An enhanced integrated aerodynamic/dynamic approach to optimum rotor blade design.” Struct. Optimization, 4, 75–44.
7.
Chattopadhyay, A., and McCarthy, T. R. (1993). “A multidisciplinary optimization approach for vibration reduction in helicopter rotor blades.” Comp. and Mathematics with Applications, 25(2), 57–72.
8.
Conway, S. (1991). “Conclusions from high‐speed rotorcraft studies.” NASA/Industry High‐Speed Rotorcraft Meeting, Am. Helicopter Soc. Aircraft Des. Committee, Phoenix, Ariz.
9.
Dollyhigh, S. M., and Sobieszczanski‐Sobieski, J. (1990). “Recent experiences with multidisciplinary analysis and optimization in advanced aircraft design.” Proc., 3rd Air Force/NASA Symp. on Recent Adv. in Multidisciplinary Anal. and Optimization, San Francisco, Calif.
10.
He, C., and Peters, D. A. (1990). “Optimization of rotor blades for combined structural, dynamic, and aerodynamic properties.” Proc., 3rd Air Force/NASA Symp. on Recent Advan. in Multidisciplinary Anal. and Optimization, San Francisco, Calif.
11.
Johnson, W. (1980). A comprehensive analytical model of rotorcraft aerodynamics and dynamics—Johnson Aeronautics version Vol II: User's Manual.
12.
Lamon, S. (1985). “XV‐15 advanced technology blade, ultimate stress analysis.” Boeing Rep. No. D210‐12345‐1.
13.
Lim, J. W., and Chopra, I. (1988). “Aeroelastic optimization of a helicopter rotor.” Proc., 44th Annu. Forum of the Am. Helicopter Soc. (AHS), Washington, D.C.
14.
(1984). “Recent experiences in multidisciplinary analysis and optimization.” NASA CP‐2327, J. Sobieszczanski‐Sobieski, ed., National Aeronautics and Space Administration (NASA), Washington D.C.
15.
Straub, F., Callahan, C. B., and Culp, J. D. (1991). “Rotor design optimization using a multidisciplinary approach.” Proc., 29th Aerosp. Sci. Meeting, Reno, Nev
16.
Sobieszczanski‐Sobieski, J. (1988). “Senstivity analysis and multidisciplinary optimization for aircraft design: recent advances and results.” 16th Congr. of Int. Council of the Aeronautical Sci., Jerusalem, Israel, 953–964.
17.
Talbot, P., Phillips, J., and Totah, J. (1990). “Selected design issues of some high speed rotorcraft concepts.” AIAA/AHS/ASEE Aircraft Des. Systems and Operations Conf., Dayton, Ohio.
18.
Vanderplaats, G. N. (1987). CONMIN—a FORTRAN program for constained function minimization: User's Manual; NASA TMX‐62282, National Aeronautics and Space Administration (NASA), Washington D.C.
19.
Weller, W. H., and Davis, M. W. (1986). “Application of design optimization techniques to rotor dynamics problems.” Proc., 42nd Annu. Forum of the Am. Helicopter Soc., (AHS), Washington, D.C., 27–44.
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Copyright © 1994 American Society of Civil Engineers.
History
Received: Nov 6, 1992
Published online: Apr 1, 1994
Published in print: Apr 1994
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