Add to ORKGThe rolling moment induced on aircraft models in the wake of a model of a subsonic transport and of a supersonic transport was measured as a function of angle of attack for several configurations. The tests are described and an analysis of the data is given in this memorandum
The results of four current analytical methods for predicting wing vortex strength and decay rate ar...
Tests were conducted in the Langley V/STOL tunnel to determine the effect of the main-rotor wake on ...
An experimental study was initiated to analyze the trajectories of the streamwise vortices behind th...
Measurements were made in the NASA-Ames 40- by 80-foot wind tunnel of the rolling moment induced on ...
A flight test investigation of the B-747 vortex wake characteristics was conducted using a T-37B as ...
A variety of fin configurations were tested on a model of the Boeing B747 in 40 by 80 foot wind tunn...
A brief exploratory flight program was conducted at Ames Research Center to investigate the vortex w...
A study is described that evaluates the accuracy of vortex-lattice methods when they are used to com...
A method is described for the prediction of rolling moments on a wing penetrating a vortex velocity ...
Simultaneous measurements were made of the upset responses experienced and the wake velocities encou...
In general, the variation of the damping-in-roll derivative with sweep angle at zero angle of attack...
A 1/8-scale model of the X-29A airplane was tested in the Ames 12-Foot Pressure Wind Tunnel at a Mac...
A research on studying the effect of the wake generated by an aircraft wing section on a following a...
PDFJournalAerodynamicsFlight dynamicsTheoremsVorticesFlowRollingAerodynamic stabilityControlUnited S...
The project completed at the Wichita State University Department of Aerospace Engineering. Presented...
The results of four current analytical methods for predicting wing vortex strength and decay rate ar...
Tests were conducted in the Langley V/STOL tunnel to determine the effect of the main-rotor wake on ...
An experimental study was initiated to analyze the trajectories of the streamwise vortices behind th...
Measurements were made in the NASA-Ames 40- by 80-foot wind tunnel of the rolling moment induced on ...
A flight test investigation of the B-747 vortex wake characteristics was conducted using a T-37B as ...
A variety of fin configurations were tested on a model of the Boeing B747 in 40 by 80 foot wind tunn...
A brief exploratory flight program was conducted at Ames Research Center to investigate the vortex w...
A study is described that evaluates the accuracy of vortex-lattice methods when they are used to com...
A method is described for the prediction of rolling moments on a wing penetrating a vortex velocity ...
Simultaneous measurements were made of the upset responses experienced and the wake velocities encou...
In general, the variation of the damping-in-roll derivative with sweep angle at zero angle of attack...
A 1/8-scale model of the X-29A airplane was tested in the Ames 12-Foot Pressure Wind Tunnel at a Mac...
A research on studying the effect of the wake generated by an aircraft wing section on a following a...
PDFJournalAerodynamicsFlight dynamicsTheoremsVorticesFlowRollingAerodynamic stabilityControlUnited S...
The project completed at the Wichita State University Department of Aerospace Engineering. Presented...
The results of four current analytical methods for predicting wing vortex strength and decay rate ar...
Tests were conducted in the Langley V/STOL tunnel to determine the effect of the main-rotor wake on ...
An experimental study was initiated to analyze the trajectories of the streamwise vortices behind th...