Brahmananda Panda

发表

Aeroelastic Stability Wind Tunnel Testing with Analytical Correlation of the Comanche Bearingless Main Rotor

Brahmananda Panda, Evhen Mychalowycz, B. Panda, 1997 .

Assembly of Finite-Element Helicopter Subsystems with Large Relative Rotations

David A. Peters, Brahmananda Panda, Jon-Shen Fuh, 1990 .

Efficient assembly of finite-element subsystems with large relative rotations. [for rotorcraft dynamic characteristics

David A. Peters, Brahmananda Panda, Jon-Shen Fuh, 1988 .

Technical Note: Assembly of Moderate-Rotation Finite Elements Used in Helicopter Rotor Dynamics

Brahmananda Panda, B. Panda, 1987 .

Technical Notes: A Robust Direct-Integration Method for Rotorcraft Maneuver and Periodic Response

Brahmananda Panda, B. Panda, 1992 .

Application of passive dampers to modern helicopters

Brahmananda Panda, Evhen Mychalowycz, Frank J Tarzanin, 1996 .

Advanced Aeroelastic Optimization Applied to an Improved Performance, Low Vibration Rotor

Brahmananda Panda, Darrell K. Young, Frank J. Tarzanin, 1999 .

Flap-Lag-Torsion Stability in Forward Flight

Inderjit Chopra, Brahmananda Panda, I. Chopra, 1985 .

Rapid analysis of flap-lag vibrarions and stability of model helicopter blades

Ranjan Vepa, Brahmananda Panda, 1981 .

Dynamic stability of hingeless and bearingless rotors in forward flight

Inderjit Chopra, Brahmananda Panda, 1986 .