Add to ORKGCollege of Engineering; Mechanical and Aerospace Engineering Department; Advisor: Dr. David Brian Landrum; Date: May 5, 2017; Pages: 14 p
This study focuses on incorporating a novel morphing rudder for a commercial transport aircraft from...
Aircraft directional stability and control are related to vertical tail design. The safety, performa...
Due to the character of the original source materials and the nature of batch digitization, quality ...
The research is an attempt to investigate the stability and controls analysis of the BD-5A aircraft,...
Results are presented of an analysis of vertical-tail shear, bending-moment, and torque loads measur...
AbstractAgeneric aircraft with the single vertical tail usually lose its directional stability at me...
The paper presents major issues associated with maneuvering of the aircraft inverted flight (acrobat...
The paper presents a new procedure to evaluate the sideforce (and hence the directional stability an...
It is the purpose of this paper to find out the effect of T-tail on Aerodynamic characteristics and ...
This report deals with the calculation of the equilibrium, statistical stability, and damping of the...
The stability analysis of the aircraft can be evaluated in two flight modes: longitudinal stabilit...
The inverted V-tail is equipped in a twin-boom UAV,whose intersection angle can influence the aerody...
Cover title."April 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliograp...
Purpose: The purpose of this research is a study into a mathematical approach of a tailless aircraft...
Work performed at Langley Research Center.N68-15941.Includes bibliographical references (p. 19).Mode...
This study focuses on incorporating a novel morphing rudder for a commercial transport aircraft from...
Aircraft directional stability and control are related to vertical tail design. The safety, performa...
Due to the character of the original source materials and the nature of batch digitization, quality ...
The research is an attempt to investigate the stability and controls analysis of the BD-5A aircraft,...
Results are presented of an analysis of vertical-tail shear, bending-moment, and torque loads measur...
AbstractAgeneric aircraft with the single vertical tail usually lose its directional stability at me...
The paper presents major issues associated with maneuvering of the aircraft inverted flight (acrobat...
The paper presents a new procedure to evaluate the sideforce (and hence the directional stability an...
It is the purpose of this paper to find out the effect of T-tail on Aerodynamic characteristics and ...
This report deals with the calculation of the equilibrium, statistical stability, and damping of the...
The stability analysis of the aircraft can be evaluated in two flight modes: longitudinal stabilit...
The inverted V-tail is equipped in a twin-boom UAV,whose intersection angle can influence the aerody...
Cover title."April 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliograp...
Purpose: The purpose of this research is a study into a mathematical approach of a tailless aircraft...
Work performed at Langley Research Center.N68-15941.Includes bibliographical references (p. 19).Mode...
This study focuses on incorporating a novel morphing rudder for a commercial transport aircraft from...
Aircraft directional stability and control are related to vertical tail design. The safety, performa...
Due to the character of the original source materials and the nature of batch digitization, quality ...