Systems and methods for controlling a magnitude of a sonic boom
作者： Donald Freund
DOI:
关键词: Sonic boom 、 Lift (force) 、 Wing twist 、 Magnitude (mathematics) 、 Aerospace engineering 、 Supersonic speed 、 Transonic 、 Acoustics 、 Engineering
摘要: A system for controlling a magnitude of sonic boom includes first sensor configured to detect condition the supersonic aircraft. The further pair wings move fore and aft. processor communicatively coupled with operatively wings. is (1) receive information from indicative condition, (2) calculate lift distribution aircraft based on information, (3) determine an existence deviation desired flight (4) control redistribute in manner that more closely conforms distribution. reduced when reduced.
lens.org 参考文章(51)
S Cheng, Device for sonic boom reduction and improving aircraft performance ,(1970)
Alan E. Arslan, John M. Morgenstern, Wing employing leading edge flaps and winglets to achieve improved aerodynamic performance ,(2005)
Richard G. Lemke, Collision avoidance system for snowmobiles ,(2004)
John M. Morgenstern, Tom Hartmann, Passive aerodynamic sonic boom suppression for supersonic aircraft ,(2000)
Victor Kenneth Stuhr, Pivoting aircraft wing and associated method ,(2004)
Chester P. Nelson, Integrated and/or modular high-speed aircraft ,(2002)
Matthew N. Mrdeza, Heinz A. Gerhardt, Joan Nolan, Kenneth Seho, Aircraft with variable forward-sweep wing ,(1998)
Richard M. Wood, Multi-body aircraft with an all-movable center fuselage actively controlling fuselage pressure drag ,(1987)
James Bach, Alan Arslan, John Morgenstern, System, apparatus, and method for redistributing forces to meet performance goals and shock wave disturbance constraints ,(2003)