Author: National Aeronautics and Space Administration (NASA)Publisher: Createspace Independent Publishing Platform
ISBN: 9781720662501
Category :
Languages : en
Pages : 72
Book Description
A piloted simulation study was performed for the purpose of indicating the noise reduction benefits and piloting performance that could occur for a typical 4-engine high-Speed Civil Transport (HSCT) configuration during takeoff when a dual thrust-cutback procedure was employed with throttle operation under direct computer control. Two thrust cutbacks were employed with the first cutback performed while the vehicle was accelerating on the run-way and the second cutback performed at a distance farther downrange. Added vehicle performance improvements included the incorporation of high-lift increments into the aerodynamic database of the vehicle and the use of limited engine oversizing. Four single-stream turbine bypass engines that had no noise suppression of any kind were used with this configuration. This approach permitted establishing the additional noise suppression level that was needed to meet Federal Air Regulation Part 36 Stage 3 noise levels for subsonic commercial jet aircraft. Noise level results were calculated with the jet mixing and shock noise modules of the Aircraft Noise Prediction Program (ANOPP).Riley, Donald R. and Glaab, Louis J. and Brandon, Jay M. and Person, Lee H., Jr. and Glaab, Patricia C.Langley Research CenterSIMULATION; TAKEOFF; AERODYNAMIC NOISE; NOISE REDUCTION; HIGH SPEED; CIVIL AVIATION; LIFT; DATA BASES; JET MIXING FLOW; COMMERCIAL AIRCRAFT; SUPERSONIC TRANSPORTS; NUMERICAL CONTROL; NOISE PREDICTION (AIRCRAFT)
