Flight and simulation investigation of methods for implementing noise-abatement landing approaches
暂无分享,去创建一个
[1] C. R. Taylor. Flight test results of a trailing edge flap designed for direct-lift control , 1969 .
[2] D. A. Hilton,et al. Variability in airplane noise measurements , 1968 .
[3] W. Willich,et al. A flight investigation of systems developed for reducing pilot workload and improving tracking accuracy during noise-abatement landing approaches , 1969 .
[4] J. W. Stickle,et al. Flight tests of a direct lift control system during approach and landing , 1968 .
[5] William C. Sperry. AIRCRAFT NOISE EVALUATION , 1968 .
[6] K. D. Kryter,et al. JUDGED NOISINESS OF A BAND OF RANDOM NOISE CONTAINING AN AUDIBLE PURE TONE. , 1965 .
[7] C. T. Jackson,et al. Validation of a research simulator for investigating jet transport handling qualities and airworthiness criteria during takeoff , 1966 .
[8] L. S. Rolls,et al. Flight-determined aerodynamic properties of a jet-augmented, auxiliary-flap, direct-lift- control system including correlation with wind-tunnel results , 1969 .
[9] K D Kryter. Concepts of perceived noisiness, their implementation and application. , 1968, The Journal of the Acoustical Society of America.