Publication | Closed Access
Static Aeroelasticity and the Flying Wing
31
Citations
7
References
1973
Year
AeroacousticsAerodynamic NoiseAirfoil Grid InletEngineeringEngineering Noise ControlNoise ControlAerospace EngineeringMechanical EngineeringStatic AeroelasticityMechanical SystemsNoise PollutionNoiseAeroelasticityAerodynamicsM. J. T.Noise ReductionAerostructureAir Mobility Noise
Smith, M. J. T. and House, M. E., Internally Generated Noise From Gas Turbine Engines, Measurement and Prediction, Transactions ofASME: Journal of Engineering for Power, 1967. Smith, E. B. et al., Study and Tests to Reduce Compressor Sounds of Jet Aircraft, TR DS-68-7, contract FA65WA-1236 to FAA, 1968, General Electric Co., Cincinnati, Ohio. Schaut, L. A., Results of an Experimental Investigation of Total Pressure Performance and Noise Reduction of an Airfoil Grid Inlet, document D6-23276, 1969, Boeing Co., Seattle, Wash.
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