𝔖 Bobbio Scriptorium

✦ LIBER ✦

Continuous Robust Control for Two-Dimensional Airfoils with Leading- and Trailing-Edge Flaps

✍ Scribed by Wang, Z.; Behal, A.; Marzocca, P.

Book ID: 121846269
Publisher: American Institute of Aeronautics and Astronautics
Year: 2012
Tongue: English
Weight: 634 KB
Volume: 35
Category: Article
ISSN: 0731-5090
DOI: 10.2514/1.54347

No coin nor oath required. For personal study only.

📜 SIMILAR VOLUMES

[American Institute of Aeronautics and A

[American Institute of Aeronautics and Astronautics 20th Fluid Dynamics, Plasma Dynamics and Lasers Conference - Buffalo,NY,U.S.A. (12 June 1989 - 14 June 1989)] 20th Fluid Dynamics, Plasma Dynamics and Lasers Conference - Global marching technique for predicting flows over airfoils with leading and trailing edge flaps

✍ HALIM, AHMAD 📂 Article 📅 1989 🏛 American Institute of Aeronautics and Astronautics ⚖ 846 KB

[American Institute of Aeronautics and A

[American Institute of Aeronautics and Astronautics 46th AIAA Aerospace Sciences Meeting and Exhibit - Reno, Nevada ()] 46th AIAA Aerospace Sciences Meeting and Exhibit - Optimum Flap Angles for Roll Control on Wings with Multiple Trailing-Edge Flaps

✍ Segawa, Hidehiro; Gopalarathnam, Ashok 📂 Article 📅 2008 🏛 American Institute of Aeronautics and Astronautics ⚖ 699 KB

[American Institute of Aeronautics and A

[American Institute of Aeronautics and Astronautics 3rd Shear Flow Conference - Orlando,FL,U.S.A. (06 July 1993 - 09 July 1993)] 3rd Shear Flow Conference - Vortex capture by a two-dimensional airfoil with a small oscillatingleading-edge flap

✍ ZHOU, M.; FERNHOLZ, H.; MA, H.; WU, J.; WU, J. 📂 Article 📅 1993 🏛 American Institute of Aeronautics and Astronautics ⚖ 461 KB

[American Institute of Aeronautics and A

[American Institute of Aeronautics and Astronautics AIAA Atmospheric Flight Mechanics Conference and Exhibit - Honolulu, Hawaii (18 August 2008 - 21 August 2008)] AIAA Atmospheric Flight Mechanics Conference and Exhibit - Flight Testing of a Model Aircraft with Trailing-Edge Flaps Optimized for Lift Distribution Control

✍ Guerreiro, Nelson; Hubbard, James 📂 Article 📅 2008 🏛 American Institute of Aeronautics and Astronautics ⚖ 369 KB

[American Institute of Aeronautics and A

[American Institute of Aeronautics and Astronautics 44th AIAA Aerospace Sciences Meeting and Exhibit - Reno, Nevada (09 January 2006 - 12 January 2006)] 44th AIAA Aerospace Sciences Meeting and Exhibit - u-Synthesis for An Active Aeroelastic Wing with Leading and Trailing Edge Control Surfaces

✍ Teng, Ying; Chen, Hsin-Piao 📂 Article 📅 2006 🏛 American Institute of Aeronautics and Astronautics ⚖ 964 KB

[American Institute of Aeronautics and A

[American Institute of Aeronautics and Astronautics 20th AIAA Computational Fluid Dynamics Conference - Honolulu, Hawaii ()] 20th AIAA Computational Fluid Dynamics Conference - Computational Model for the Dynamic Analysis of a Two-Dimensional Airfoil with a Control Surface

✍ Jiménez, Rodrigo; Lopez, Omar 📂 Article 📅 2011 🏛 American Institute of Aeronautics and Astronautics ⚖ 731 KB