Add to ORKGIn this method, the gust velocities are represented as rolling gusts, yawing gusts, and side gusts. Random distributions of gust velocities across the span are taken into account in defining the rolling and yawing gusts. Complex stability derivatives are used to account for the random distribution of side gusts along the fuselage and vertical tail and the lag effects in gust penetration. A sample calculation procedure is presented for obtaining the response of the airplane in each degree of freedom
This report presents the results of an analytical study of the lateral controllability of an airplan...
The effect of spanwise variations in gust intensity on the power spectrum directly due to atmospheri...
Graphs and formulas are given with the aid of which all the aerodynamic coefficients required for co...
The report is separated into two parts. In the first part the theoretical basis for calculating the ...
The statistical approach to the gust-load problem which consists in considering flight through turbu...
The statistical approach to the gust-load problem which consists in considering flight through turbu...
In this method, the gust velocities are represented as rolling gusts, yawing gusts, and side gusts. ...
A method of computing the power spectral densities of the lateral response of airplanes to random at...
Distributed lateral motions have been calculated for a hypothetical small airplane with various modi...
An investigation was made to determine the accuracy with which the lateral flight motions of a swept...
The correlation functions and power spectra of the rolling and yawing moments on an airplane wing du...
A theory is presented for calculating the variation with frequency of the lateral-force and yawing-m...
The statistical approach to the gust-load problem, which consists in considering flight through turb...
A method is presented for estimating some lateral and longitudinal rigid-body responses of airplanes...
The statistical approach to the gust-load problem which consists in considering flight through turbu...
This report presents the results of an analytical study of the lateral controllability of an airplan...
The effect of spanwise variations in gust intensity on the power spectrum directly due to atmospheri...
Graphs and formulas are given with the aid of which all the aerodynamic coefficients required for co...
The report is separated into two parts. In the first part the theoretical basis for calculating the ...
The statistical approach to the gust-load problem which consists in considering flight through turbu...
The statistical approach to the gust-load problem which consists in considering flight through turbu...
In this method, the gust velocities are represented as rolling gusts, yawing gusts, and side gusts. ...
A method of computing the power spectral densities of the lateral response of airplanes to random at...
Distributed lateral motions have been calculated for a hypothetical small airplane with various modi...
An investigation was made to determine the accuracy with which the lateral flight motions of a swept...
The correlation functions and power spectra of the rolling and yawing moments on an airplane wing du...
A theory is presented for calculating the variation with frequency of the lateral-force and yawing-m...
The statistical approach to the gust-load problem, which consists in considering flight through turb...
A method is presented for estimating some lateral and longitudinal rigid-body responses of airplanes...
The statistical approach to the gust-load problem which consists in considering flight through turbu...
This report presents the results of an analytical study of the lateral controllability of an airplan...
The effect of spanwise variations in gust intensity on the power spectrum directly due to atmospheri...
Graphs and formulas are given with the aid of which all the aerodynamic coefficients required for co...