Flight testing a highly flexible aircraft - Case study on the MIT Light Eagle
Author:
Affiliation:
1. MIT, Cambridge, MA
2. NASA, Flight Research Center, Edwards, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1988-4375
Reference6 articles.
1. Petre A., Ashley H.; Drag Effects on Wing Flutter; Journalof Aircraft;Vol. 13;No. 10;October 1976;pp. 755-763
2. Cheng G.S.;Aeroelastic Behavior of Forward Swept GraphiteIEpoxyWing Aircraft with Rigid-BodyFreedoms; Ph.D ThesisMassachusettsInstituteofTechnology;TELAC Report 86-14;May 1986
Cited by 4 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Evolution of flight vehicle system identification;Journal of Aircraft;1996-01
2. Identification of actuation system and aerodynamic effects of direct-lift-control flaps;Journal of Aircraft;1993-09
3. Aeroelastic characteristics of a highly flexible aircraft;Journal of Aircraft;1990-10
4. The flight control system for the Daedalus human powered aircraft;Guidance, Navigation and Control Conference;1989-08-14
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