A Method for Computing Rotary Wing Airload Distribution Iin Forward FlightCornell Aeronautical Laboratory1962ZIP
Effect of Structural Flexibiligy on Aircraft Loading. Part II, Spanwise Airload DistributionTheodore Pian1951ZIP
A Full Potential Flow Analysis with Realistic Wake Influence for Helicopter Rotor Airload Prediction / T. Alan Egolf and S. Patrick Sparks.T. Alan. Egolf1987ZIP
Effect of Structural Flexibiligy on Aircraft Loading. Part V, Rapid Estimation of Some Effects of Aeroelasticity on Airload Distribution at an Abrupt Aileron DistributionTheodore Pian1952ZIP
Effect of Structural Flexibiligy on Aircraft Loading. Part VI, An Approximate Method for Determining Spanwise Airload Distribution Over an Elastic Wing in Subsonic FlowHua Lin1952ZIP
Effect of Structural Flexibiligy on Aircraft Loading. Part VIII, Symmetric Airload Distribution Over a Thin Elastic Delta Wing with Subsonic Leading Edge at Supersonic SpeedHua Lin1953ZIP