Add to ORKGRandom numbers were generated with the aid of a digital computer and transformed such that the probability density function of a discrete random load history composed of these random numbers had one of the following non-Gaussian distributions: Poisson, binomial, log-normal, Weibull, and exponential. The resulting random load histories were analyzed to determine their peak statistics and were compared with cumulative peak maneuver-load distributions for fighter and transport aircraft in flight
A non-Gaussian model of atmospheric turbulence is presented and analyzed. The model is restricted to...
Methods are presented for calculating design limit loads compatible with probabilistic structural de...
The combined load statistics are developed by taking the acoustically induced load to be a random po...
Random numbers were generated with the aid of a digital computer and transformed such that the proba...
Statistical prediction of aircraft maneuver fatigue loads from eight-channel oscillograph flight dat
Airplanes.Uunder the assumpiton that the operational gust or gust-load history of an airplane is a G...
The feasibility of conducting a statistical analysis of simulation experiments to study airport capa...
A method is described for generating time histories which model the frequency content and certain no...
Power spectral densities of normal load factor have been obtained for two service operational traini...
Three random number generators, which produce Gaussian white noise sequences, were compared to asses...
The random process used to model atmospheric turbulence in aircraft response problems is examined. T...
Methods are presented for calculating design limit loads compatible with probabilistic structural de...
A major task of the program to develop an expert system to predict the loads on selected components ...
This study addresses the growing need for appropriate methods of analysis and simulation of service ...
This paper treats the theoretical fatigue analysis of non-Gaussian random loadings. It first reviews...
A non-Gaussian model of atmospheric turbulence is presented and analyzed. The model is restricted to...
Methods are presented for calculating design limit loads compatible with probabilistic structural de...
The combined load statistics are developed by taking the acoustically induced load to be a random po...
Random numbers were generated with the aid of a digital computer and transformed such that the proba...
Statistical prediction of aircraft maneuver fatigue loads from eight-channel oscillograph flight dat
Airplanes.Uunder the assumpiton that the operational gust or gust-load history of an airplane is a G...
The feasibility of conducting a statistical analysis of simulation experiments to study airport capa...
A method is described for generating time histories which model the frequency content and certain no...
Power spectral densities of normal load factor have been obtained for two service operational traini...
Three random number generators, which produce Gaussian white noise sequences, were compared to asses...
The random process used to model atmospheric turbulence in aircraft response problems is examined. T...
Methods are presented for calculating design limit loads compatible with probabilistic structural de...
A major task of the program to develop an expert system to predict the loads on selected components ...
This study addresses the growing need for appropriate methods of analysis and simulation of service ...
This paper treats the theoretical fatigue analysis of non-Gaussian random loadings. It first reviews...
A non-Gaussian model of atmospheric turbulence is presented and analyzed. The model is restricted to...
Methods are presented for calculating design limit loads compatible with probabilistic structural de...
The combined load statistics are developed by taking the acoustically induced load to be a random po...