In order to provide engineers interested in rotating-wing aircraft, but with no specialized training in stability theory, some understanding of the factors that influence the flying qualities of the helicopter, an explanation is made of both the static stability and the stick-fixed oscillation in hovering and forward flight in terms of fundamental physical quantities. Three significant stability factors -- static stability with angle of attack, static stability with speed, and damping due to a pitching or rolling velocity -- are explained in detail
This article provides an introduction to Section 5.1 on flight mechanics and dynamics, stability an...
The analytical capability of the helicopter stability program is discussed. The parameters which are...
Basic Helicopter Aerodynamics is widely appreciated as an easily accessible, rounded introduction to...
In order to provide engineers interested in rotating-wing aircraft, but with no specialized training...
A brief summary is made of methods available to the helicopter designer for obtaining desired stabil...
Theoretical and experimental developments in the aeroelastic and aeromechanical stability of helicop...
The present report deals with a number of the main problems requiring solution in the development of...
The present report is a study of the dynamic stability of a helicopter with hinged rotor blades unde...
Since the author has always been interested in Aeronautical Engineering, and in particular, rotary-w...
Flight-test measurements, related analytical studies, and corresponding pilots' opinions of the spee...
A theoretical analysis of helicopter maneuver stability is made and the results are compared with ex...
This book gives an account from first principles of the aerodynamics of helicopter flight, concentra...
The stability and control of rotors at high advance ratio are considered. Teetering, articulated, gi...
Basic Helicopter Aerodynamics is widely appreciated as an easily accessible, rounded introduction to...
The results of an analytical study aimed at predicting the aeromechanical stability of a helicopter ...
This article provides an introduction to Section 5.1 on flight mechanics and dynamics, stability an...
The analytical capability of the helicopter stability program is discussed. The parameters which are...
Basic Helicopter Aerodynamics is widely appreciated as an easily accessible, rounded introduction to...
In order to provide engineers interested in rotating-wing aircraft, but with no specialized training...
A brief summary is made of methods available to the helicopter designer for obtaining desired stabil...
Theoretical and experimental developments in the aeroelastic and aeromechanical stability of helicop...
The present report deals with a number of the main problems requiring solution in the development of...
The present report is a study of the dynamic stability of a helicopter with hinged rotor blades unde...
Since the author has always been interested in Aeronautical Engineering, and in particular, rotary-w...
Flight-test measurements, related analytical studies, and corresponding pilots' opinions of the spee...
A theoretical analysis of helicopter maneuver stability is made and the results are compared with ex...
This book gives an account from first principles of the aerodynamics of helicopter flight, concentra...
The stability and control of rotors at high advance ratio are considered. Teetering, articulated, gi...
Basic Helicopter Aerodynamics is widely appreciated as an easily accessible, rounded introduction to...
The results of an analytical study aimed at predicting the aeromechanical stability of a helicopter ...
This article provides an introduction to Section 5.1 on flight mechanics and dynamics, stability an...
The analytical capability of the helicopter stability program is discussed. The parameters which are...
Basic Helicopter Aerodynamics is widely appreciated as an easily accessible, rounded introduction to...