Source Information

 

Moishe Garfinkle        garfinkm@mail.drexel.edu

Christopher Pastore      pastorec@philau.edu

M. Garfinkle - United States Patent 5,269,657 Aerodynamically Stable Airfoil Spar; Dec 1993 - All rights Reserved

E. S. Greenhalgh, C. Pastore and M. Garfinkle, A Continuous-Fiber Composite Wing Box-Beam Exhibiting Twist-Beam Coupling;

Composite Engineering; 3(1993)691

 

E. S. Greenhalgh, C. Pastore and M. Garfinkle, Aeroelastic Smart Spar;

Composite Manufacturing; 4(1993)195

 

A. Bogdanovich, C. Pastore, E. Greenhalgh & Birger; Analytical and Experimental Results for a Quasi-Unbalanced Composite Double Box Beam Spar;

Proc. Am. Soc. for Composites, 8th Tech. Conf. Cleveland, ON Oct 95

J. Allburn, J. Retelle, J. Krone & W. Lamar; X-29 Revives the Experimental Aircraft;

AIA Aerospace America, Feb. 1986; p 30

 

H. Atanasoff & A. Vizzini - A Mfg. Process for Open-Mold Mechanically Coupled Composite Box Beams with Foam Tooling; AIAA/ASME/AHS/ASC, 28th Structures, Structural Dynamics & Materials Conf.1989

 

L. Corso, D. Popelka & M. Nixon; Design, Analysis and Test of a Composite Tailored Tiltrotor Wing; Am. Helicopter Soc., 53rd Annual Forum; Virginia Beach, VA; 29 Apr 97

 

L. Clements; Adhesive Bonding Used in Wing Torque Box; High-Performance Composites, May/June, 1999; p 80

 

M. Goorjian, E. Tu & G. Guruswamy; Aeroelastic Computations for Wings with Preloaded Tips; Ames Research Center; NASA Tech Brief ARC-11753

 

 

M. Shirk, T. Hertz & T. Weisshaar; Aeroelastic Tailoring - Theory, Practice and Promise;

J. Aircraft; 23(1984)6