License A & C
1.1 Module Note
1.1.1 Theory of flight ( stability )
Rolling stability :
1. Dihedral angle.
2. Sweepback wings.
3. High fin.
4. High wings and lows center of gravity.
Directional stability :1. Vertical fin.
EFFECT OF CANARD DEFLECTION ON CLOSE-COUPLED
Eugene L. Th *
NASA Ames Research Center
Moffett Field, California 94035
Downloaded by Beihang University on December 7, 2012 | http:/arc.aiaa.org | DOI
EFFECT OF CANARD DEFLECTION ON ENHANCED LIFT
FOR A CLOSE-COUPLED-CANARD CONFIGURATION
Richard M. Howardt and John M. Kersh, Jr.5
Naval Postgraduate School, Monterey, California
maneuver in a mimimum time, or by holding a
flight condition fo
AIAA Atmospheric Flight Mechanics Conference and Exhibit
15 - 18 August 2005, San Francisco, California
Optimal Location and Size of Canards for Aeroelastic
Actuation in Aerospace Vehicles
Downloaded by Beihang University on December 7, 201