A DESIGN OPTIMIZATION PROCEDURE FOR MINIMIZING DRIVE SYSTEM WEIGHT OF HIGH SPEED PROP-ROTORS

References

• Talbot , P. , Phillips , J. and Totah , J. ( 1990 ) Selected Design Issues or Some High Speed Rotorcraft Concepts . AIAA/AHS/ASEE Aircraft Design, Systems and Operations Conference , September 17-19 , Dayton , Ohio .
   Google Scholar
• Conway , S. ( 1991 ) Conclusions from High speed Rotorcraft Studies . NASA/Industry High speed Rotorcraft Meeting , May 8 , Phoenix , Arizona .
   Google Scholar
• Wilkerson , J. B. , Schneider , J. J. , and Bartic , K. M. ,( 1991 ) Technology Needsfor Highspeed Rotorcraft (I) . NASA CR 177585 .
   Google Scholar
• Schoen , A. H. , et al. ( 1980 ) User's Manualfor VASCOMP II, V/STOL Aircraft Sizing and Performance Computer Program . Boeing Vertol Company , Report d8-0375 , Volume IV .
   Google Scholar
• Arrington , W. L. , Kumpel , M. , Marr , R. L. and McEntire , K. G. ( 1985 ) XV-15 Tilt Rotor Research Aircraft Flight Test Data Report . NASA CR 177406 .
   Google Scholar
• Vanderplaals , G. N. ( 1973 ) CON MIN-A Fortran Programfor Constrained Function Minimization, User's Manual . NASA TMX-62282 .
   Google Scholar
• Fadel , G M. , Riley , M. F. and Barthelemy , J. M. ( 1988 ) Two Point Exponential Approximation method for Structural Optimization . Structural Optimization , 2 , 117 – 224 .
   Google Scholar
• McCarthy , T. R. and Chattopadhay , A. ( 1993 ). Design of High Speed Proprotors Using Multiobjective Optimization Techniques . Paper No. AIAA 93-1032,AIAA/AHS/ASEE Aerospace Design Conference , Irvine , California , February 16-19 .
   Google Scholar
• Johnson , W. ( 1988 ) A Comprehensive Analytical Model ofRotorcraft Aerodynamics and Dynamics-Johnson Aeronautics Version . Vol. II . User's Manual .
   Google Scholar