Zobrazeno 1 - 10
of 82
pro vyhledávání: '"Terrence A. Weisshaar"'
Publikováno v:
Journal of Aircraft. 51:727-739
Reconfigurable aircraft are capable of in-flight shape change to increase mission performance or provide multimission capability. This paper examines a fundamental issue raised by aircraft reconfigurability: design of an optimal, lightweight structur
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::561a6455b9ea45dc57f1b76d04441da6
https://doi.org/10.2514/1.c032427
https://doi.org/10.2514/1.c032427
Autor:
Terrence A. Weisshaar
Publikováno v:
Journal of Aircraft. 50:337-353
The term ‘morphing aircraft’ describes a broad range of air vehicles and vehicle components that adapt to planned and unplanned multipoint mission requirements. Adaptation or morphing requires changing system features including vehicle ‘states,
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::61b596503f7251ebf5fafde19f2271b1
https://doi.org/10.2514/1.c031456
https://doi.org/10.2514/1.c031456
Publikováno v:
Journal of Aircraft. 50:615-625
An alternative to vertical tails, wing-tip fins, a type of winglet, provide yaw stability and control and some operational and maintenance advantages. Winglets reduce wing-induced drag but may reduce flutter speed, requiring wing stiffening and a str
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f7aa2d7f4c7bd9b9981bf78cca9dd04a
https://doi.org/10.2514/1.c031978
https://doi.org/10.2514/1.c031978
Autor:
Terrence A. Weisshaar, David K. Duke
Publikováno v:
Journal of Aircraft. 43:157-164
This paper describes the use of full-span deforming control surfaces (including controlled chordwise cambering of the wing) to provide effective subsonic induced drag control with precise control of the spanwise lift distribution. Examples of these p
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::461157cc3fc42448f315750df7c81ded
https://doi.org/10.2514/1.12040
https://doi.org/10.2514/1.12040
Autor:
Eli Livne, Terrence A. Weisshaar
Publikováno v:
Journal of Aircraft. 40:1047-1065
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::65312484b1f5be56573d11982c2d7598
https://doi.org/10.2514/1.2273
https://doi.org/10.2514/1.2273
Publikováno v:
Journal of Aircraft. 39:227-233
Reducing aircraft design cycle time while improving product quality requires improved information e ow, process optimization, and use of advanced computational methods, including optimization, at critical times during the design process. Computer tec
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fd620e75ff72019b30a39eac0a3e5f51
https://doi.org/10.2514/2.2943
https://doi.org/10.2514/2.2943
Publikováno v:
Smart Materials and Structures. 5:216-224
The purpose of this work is to design an active control system for flutter suppression of a laminated plate wing model using segmented piezo-actuators. We describe investigations pertaining to the optimal size, thickness and locations of piezo-actuat
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a63e0c7037d39c1080261d043494dbac
https://doi.org/10.1088/0964-1726/5/2/010
https://doi.org/10.1088/0964-1726/5/2/010
Autor:
Terrence A. Weisshaar, Robert C. Scott
Publikováno v:
Journal of Aircraft. 31:213-222
Piezoelectrics and shape memory alloys may be used as integrated actuators to control supersonic flutter of flat panels because panel strain and stiffness can be actively controlled. This article uses a Rayleigh Ritz panel flutter model to analyze th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::064624e1d4626d20da0a9f30be506459
https://doi.org/10.2514/3.46476
https://doi.org/10.2514/3.46476
Autor:
Shinji Suzuki, Terrence A. Weisshaar
Publikováno v:
Journal of the Japan Society for Aeronautical and Space Sciences. 42:455-461
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3796bf74a884ec7cfaf3c21334cd9fdc
https://doi.org/10.2322/jjsass1969.42.455
https://doi.org/10.2322/jjsass1969.42.455
Publikováno v:
Journal of Aircraft. 30:534-540
Piezoelectric actuators are embedded in an idealized laminated composite wing structure that can adapt to changing flight conditions. A feedback control system senses wing roots strains and then applies a proportional voltage to active actuator layer
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::84e8dd8d71955949d1bee7265e3c2c2d
https://doi.org/10.2514/3.46376
https://doi.org/10.2514/3.46376