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Acoustic Feedback and Its Impact on Fan Flutter in Short Aeroengine Intakes
Acoustic Liner Feasibility Program Final Report, 19 Nov. 1968 - 19 Apr. 1970
ACSYNT inner loop flight control design study
Active aeroelastic control with time delay for targeted flutter modes
Active and Natural Suction at Forward-Facing Steps for Delaying Laminar–Turbulent Transition
Active and passive vortex wake mitigation using control surfaces
Active camber system for lateral stability improvement of urban vehicles
Active control landing gear for ground loads alleviation
Active control of aerothermoelastic effects for a conceptual hypersonic aircraft
Active control of aerothermoelastic effects for a conceptual hypersonic aircraft
Active control of aerothermoelastic effects for a conceptual hypersonic aircraft
Active control of gust- and interference-induced vibration of tilt-rotor aircraft
Active Control of Noise from Hot Supersonic Jets
Active Control of Separation From the Flap of a Supercritical Airfoil
Active Control of Surge in Multi-Stage Axial-Flow Compressors
Active Control of Vehicle Handling Dynamics
Active control of wing rock of a delta wing at post-stall using tangential leading edge blowing
Active controls technology to maximize structural efficiency
Active control technology and the use of multiple control surfaces
Active control technology experience with the Space Shuttle in the landing regime
Active Control Technology Experience with the Space Shuttle in the Landing Regime
Active Dihedral Control System for a Torisionally Flexible Wing
Active Dihedral Control System for a Torsionally Flexible Wing
Active external store flutter suppression in the YF-17 flutter model
Active Flexible Wing Aeroservoelastic Wind-Tunnel Test Program
Active Flow Control at Low Reynolds Numbers on a NACA 0015 Airfoil
Active flutter control for flexible vehicles, volume 1
Active flutter suppression - Control system design and experimental validation
Active flutter suppression using eigenspace and linear quadratic design techniques
Active flutter suppression using eigenspace and linear quadratic design techniques
Active flutter suppression using invariant zeros/eigensystem assignment