@conference {1432, title = {1432. Potential Benefits of Integrated Active Controls Systems for Current Technology Commercial Transports}, booktitle = {40th Annual Conference, Dayton, Ohio, May 4-7}, year = {1981}, note = {

L. R. "Mike" Hackney Award

}, month = {5/4/81}, pages = {55}, publisher = {Society of Allied Weight Engineers, Inc.}, organization = {Society of Allied Weight Engineers, Inc.}, type = {10. WEIGHT ENGINEERING - AIRCRAFT DESIGN}, address = {Dayton, Ohio}, abstract = {

This paper summarizes the definition of five current technology commercial transport airplanes with integrated active controls systems. Their potential performance and economic improvements relative to a Conventional Baseline Airplane are presented. Weight assessments of active controls functions, a summary of the wing structure detailed weight analysis,and center-of-gravity management (balance and loadabi1ity) data are also discussed. *This paper reports work accomplished under NASA contracts NAS1-14742 and NAS1-15325. Acknowledgment is made to Robert H. Brunelle, Albert E. Chukitus, Keith H. Hartz, Robert A. McManus, and the IAAC Design Team, who provided data and guidance.

}, keywords = {10. Weight Engineering - Aircraft Design, Mike Hackney Best Paper Award}, url = {https://www.sawe.org/papers/1432/buy}, author = {Brown, J D and Thomas, C J} }