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  • Test and Evaluation of Fuselage Vibration Utilizing Active Control of Structural Response (ACSR) Optimized to ADS-27 Member price: $15.00 $30.00
  • An Experimental and Analytical Investigation of Dynamic Stall Effects on Isolated Rotor Flap-Lag Stability Member price: $15.00 $30.00
  • Development of UMARC (University of Maryland Advanced Rotorcraft Code) Member price: $15.00 $30.00
  • On Chaos Methods Applied to Higher Harmonic Control Member price: $15.00 $30.00
  • Frequency-Response Method for Rotorcraft System Identification with Applications to the BO-105 Helicopter Member price: $15.00 $30.00
  • Finite Element Model Reduction Application to Parametric Studies and Optimization of Rotorcraft Structures Member price: $15.00 $30.00
  • Validation of a New General Aerospatiale Aeroelastic Rotor Model Through the Wind Tunnel and Flight Tests Data Member price: $15.00 $30.00
  • A Modal-Based Procedure for Efficiently Predicting Low Vibration Rotor Designs Member price: $15.00 $30.00
  • Application of Nonlinear Programming Techniques to Dynamic Correlation and Design of Helicopter Structures Member price: $15.00 $30.00
  • Nonlinear Coupled Rotor-Fuselage Helicopter Vibration Studies with Higher Harmonic Control Member price: $15.00 $30.00
  • Hingeless Rotor Blade Stability Using a Coupled Aeroelastic Analysis with Refined Aerodynamic Modeling Member price: $15.00 $30.00
  • An Enhanced Integrated Aerodynamic Load/Dynamic Approach to Optimum Rotor Blade Design Member price: $15.00 $30.00

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