The takeoff and approach performance of an aircraft is calculated in accordance with the airworthiness standards of the Federal Aviation Regulations. The aircraft and flight constraints are represented in sufficient detail to permit realistic sensitivity studies in terms of either configuration modifications or changes in operational procedures. The program may be used to investigate advanced operational procedures for noise alleviation such as programmed throttle and flap controls. Extensive profile time history data are generated and are placed on an interface file which can be input directly to the NASA aircraft noise prediction program (ANOPP)
A set of computer programs has been developed to estimate the takeoff and initial climb-out maneuver...
IBM 7094 digital program using steepest ascent technique for optimizing flight path of supersonic tr...
A computer technique to determine the mission radius and maneuverability characteristics of combat a...
Federal Aviation Administration2017PDFTech ReportThomas, JacquelineHansman, R. JohnUnited States. Fe...
Minimizing performance criterion to analyze ability of automatically controlled aircraft to maintain...
Thesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 201...
Calculation procedures are presented for predicting the noise-time histories and noise contours (foo...
Piloted-simulator studies were conducted to determine takeoff and landing operating procedures for a...
A user's manual is presented for a computer program for predicting the performance (static, flight, ...
A systems analysis was performed with experimental jet noise data, engineaircraft performance codes ...
Climbout and landing approach noise measurements for three engine turbofan transport aircraf
Analyses of McDonnell Douglas DC-8, DC-9, and DC-10 jet transports were conducted to investigate the...
Calculation procedures are presented for predicting maximum passby noise levels and contours (footpr...
NASA computer codes in the areas of preliminary sizing and enroute performance, takeoff and landing ...
The development and testing of a real-time takeoff performance monitoring system is discussed. The a...
A set of computer programs has been developed to estimate the takeoff and initial climb-out maneuver...
IBM 7094 digital program using steepest ascent technique for optimizing flight path of supersonic tr...
A computer technique to determine the mission radius and maneuverability characteristics of combat a...
Federal Aviation Administration2017PDFTech ReportThomas, JacquelineHansman, R. JohnUnited States. Fe...
Minimizing performance criterion to analyze ability of automatically controlled aircraft to maintain...
Thesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 201...
Calculation procedures are presented for predicting the noise-time histories and noise contours (foo...
Piloted-simulator studies were conducted to determine takeoff and landing operating procedures for a...
A user's manual is presented for a computer program for predicting the performance (static, flight, ...
A systems analysis was performed with experimental jet noise data, engineaircraft performance codes ...
Climbout and landing approach noise measurements for three engine turbofan transport aircraf
Analyses of McDonnell Douglas DC-8, DC-9, and DC-10 jet transports were conducted to investigate the...
Calculation procedures are presented for predicting maximum passby noise levels and contours (footpr...
NASA computer codes in the areas of preliminary sizing and enroute performance, takeoff and landing ...
The development and testing of a real-time takeoff performance monitoring system is discussed. The a...
A set of computer programs has been developed to estimate the takeoff and initial climb-out maneuver...
IBM 7094 digital program using steepest ascent technique for optimizing flight path of supersonic tr...
A computer technique to determine the mission radius and maneuverability characteristics of combat a...