Add to ORKGSummarized are the aerodynamic center, alpha and q- aeroelastic effects on fighter-type aircraft in the 18,700 N gross range. The results indicate that with proper tailoring of planform (fixed or variable sweep), stiffner and elastic axis location it is possible to minimize trim requirements between selected extreme conditions. The inertial effects were found to be small for this class of aircraft
An experimental investigation has been made to determine the static stability characteristics of thr...
A theoretical analysis has been made of the effects of aeroelasticity on the static longitudinal sta...
The experimental longitudinal and lateral-directional stability characteristics of a Langley concept...
An explanation is presented of the method used to locate the elastic axis and the method to determin...
This paper discusses the trends in longitudinal dynamic aeroelastic stability of a generic x-wing ai...
Expressions are derived for computing the aerodynamic influence coefficient matrix for nonplanar win...
The method used in computing the structural influence coefficient matrix of the computer program of ...
The procedures used to establish the mass matrices characteristics for the fighter type wings studie...
The computer program used to determine the rigid and elastic stability derivatives presented in the ...
Stability derivatives for predicting stability characteristics of elastic aircraf
Comprehensive aeroelastic analyses and wind tunnel tests have been conducted on a model of a typical...
A theoretical analysis of the effects of aeroelasticity on the stick-fixed static longitudinal stabi...
This report gives the results of pressure-distribution tests made to study the effects on lateral st...
The structural design of flight vehicles is a balancing act between maximizing loading capability wh...
The distribution of flight loads on an aircraft structure determine the lift and pitching moment cha...
An experimental investigation has been made to determine the static stability characteristics of thr...
A theoretical analysis has been made of the effects of aeroelasticity on the static longitudinal sta...
The experimental longitudinal and lateral-directional stability characteristics of a Langley concept...
An explanation is presented of the method used to locate the elastic axis and the method to determin...
This paper discusses the trends in longitudinal dynamic aeroelastic stability of a generic x-wing ai...
Expressions are derived for computing the aerodynamic influence coefficient matrix for nonplanar win...
The method used in computing the structural influence coefficient matrix of the computer program of ...
The procedures used to establish the mass matrices characteristics for the fighter type wings studie...
The computer program used to determine the rigid and elastic stability derivatives presented in the ...
Stability derivatives for predicting stability characteristics of elastic aircraf
Comprehensive aeroelastic analyses and wind tunnel tests have been conducted on a model of a typical...
A theoretical analysis of the effects of aeroelasticity on the stick-fixed static longitudinal stabi...
This report gives the results of pressure-distribution tests made to study the effects on lateral st...
The structural design of flight vehicles is a balancing act between maximizing loading capability wh...
The distribution of flight loads on an aircraft structure determine the lift and pitching moment cha...
An experimental investigation has been made to determine the static stability characteristics of thr...
A theoretical analysis has been made of the effects of aeroelasticity on the static longitudinal sta...
The experimental longitudinal and lateral-directional stability characteristics of a Langley concept...