Miller, G.D., "Active Flexible Wing (AFW) Technology," Air Force Wright Aeronautical Laboratories TR-87-3096, February, 1988.
Miller, G.D., "AFW Design Methodology Study", Rockwell-Aerospace Report No. NA 94-1731, December 1994.
Pendleton, E., Griffin, K., Kehoe, M., and Perry, B., "A Flight Research Program for Active Aeroelastic Wing Technology," Paper 96-1574, Proceedings of the 37th AIAA Structures, Structural Dynamics, and Materials Conference, Salt Lake City, Utah, 15–ngày 17 tháng 4 năm 1996.
Zillmer, S., "Integrated Structure / Maneuver Design Procedure for Active Aeroelastic Wings, User’s Manual," Wright Laboratory TR-97-3087, March, 1997.
Pendleton, E., Bessette, D., Field P., Miller, G., and Griffin, K., "Active Aeroelastic Wing Flight Research Program: Technical Program & Model Analytical Development," Journal of Aircraft, Volume 37, Number 4, July–August, 2000.
Pendleton, E., " Active Aeroelastic Wing," AFRL Technology Horizons, Selected Science and Technology Articles, Vol. 1, No. 2, June 2000.
Pendleton, E., "How Active Aeroelastic Wings are a Return to Aviation’s Beginning and a Small Step to Future Bird-like Wings," Invited Paper, Japan Society of Aeronautical and Space Sciences Aircraft Symposium, Sendai, Japan, ngày 11 tháng 10 năm 2000.
The Boeing Company, "The Active Aeroelastic Wing Flight Research Program (The X-53) Final Report", Volume 1 and II, AFRL-VA-WP-TR-2005-3082, October, 2005.
Pendleton, E., Flick, P., Voracek, D., Reichenbach, E., Griffin, K., Paul, D.,"The X-53,A Summary of the Active Aeroelastic Wing Flight Research Program," Paper 07-1855, Proceedings of the 48th AIAA Structures, Structural Dynamics, and Materials Conference, Honolulu, Hawaii, April 23–26, 2007.
