A new look at arbitrary motion unsteady aerodynamics and its application to rotary-wing aeroelasticity
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[1] Peretz P. Friedmann,et al. New approach to finite-state modeling of unsteady aerodynamics , 1986 .
[2] P. Friedmann,et al. Finite-time arbitrary-motion unsteady cascade airfoil theory for helicopter rotors in hover , 1985 .
[3] Peretz P. Friedmann,et al. Coupled helicopter rotor/body aeromechanical stability comparison oftheoretical and experimental results , 1985 .
[4] Peretz P. Friedmann,et al. Application of the finite-state arbitrary-motion aerodynamics to rotor blade aeroelastic response and stability in hover and forward flight , 1985 .
[5] Sesi Kottapalli,et al. Technical Notes: Unsteady Aerodynamics of Oscillating Airfoils with Inplane Motions , 1985 .
[6] Peretz P. Friedmann,et al. Unsteady aerodynamics in time and frequency domains for finite time arbitrary motion of rotary wings in hover and forward flight , 1984 .
[7] Peretz P. Friedmann,et al. Influence of various unsteady aerodynamic models on the aeromechanical stability of a helicopter in ground resonance , 1984 .
[8] Peretz P. Friedmann,et al. Formulation and solution of rotary-wing aeroelastic stability and response problems , 1983 .
[9] Wayne Johnson,et al. Influence of unsteady aerodynamics on hingeless rotor ground resonance , 1982 .
[10] Wayne Johnson,et al. Comparison of calculated and measured helicopter rotor lateral flapping angles , 1981 .
[11] William G. Bousman,et al. An Experimental Investigation of the Effects of Aeroelastic Couplings on Aeromechanical Stability of a Hingeless Rotor Helicopter , 1981 .
[12] E. H. Dowell,et al. A simple method for converting frequency domain aerodynamics to the time domain , 1980 .
[13] David A. Peters,et al. Theoretical prediction of dynamic inflow derivatives , 1980 .
[14] David A. Peters,et al. Theoretical Flap-Lag Damping With Various Dynamic Inflow Models , 1980 .
[15] D. Banerjee,et al. Parameter identification applied to analytic hingeless rotor modeling , 1979 .
[16] R. Vepa,et al. On the use of Pade approximants to represent unsteady aerodynamic loads for arbitrarily small motions of wings , 1976 .
[17] K. W. Shipman,et al. A Two-Dimensional Theory for Rotor Blade Flutter in Forward Flight , 1971 .
[18] Katsuhiko Ogata,et al. Modern Control Engineering , 1970 .
[19] R. Loewy. A Two-Dimensional Approximation to the Unsteady Aerodynamics of Rotary Wings , 1957 .
[20] Paul J Carpenter,et al. Effect of a Rapid Blade-Pitch Increase on the Thrust and Induced-Velocity Response of a Full-Scale Helicopter Rotor , 1953 .
[21] R. T. Jones. The unsteady lift of a wing of finite aspect ratio , 1940 .
[22] T. Theodorsen. General Theory of Aerodynamic Instability and the Mechanism of Flutter , 1934 .