Add to ORKGWind tunnel investigation of drag and static stability characteristics of four helicopter fuselage model
Modern rotorcrafts are subjected to some of the most complex flow behaviors ever encountered by the ...
A wind-tunnel investigation was conducted to determine the effects of the main-rotor wake on the aer...
The problem of rotor-fuselage aerodynamic interaction has to be considered in industry applications ...
Longitudinal aerodynamic characteristics of two full-scale helicopter fuselage model
An investigation was conducted in the Langley full-scale tunnel to determine the drag characteristic...
Experimental data are presented for the parasite drag of various helicopter fuselage components, suc...
The present paper describes results of wind tunnel experiments obtained during a research programme ...
Experimental aerodynamic investigations remain the subject of interest in rotorcraft community since...
An investigation has been conducted in the Langley full-scale tunnel to determine the parasite drag ...
Wind-tunnel tests of a heavy-class helicopter model were carried out to evaluate the effectiveness o...
Results of a wind tunnel test campaign to assess technologies for improvement of helicopter fuselage...
Rough conventional, smooth conventional, and laminar-flow or low-drag sections were tested. The item...
An investigation was made in the Langley V/STOL tunnel to determine rotor induced effects on a 1/4-s...
An exploratory wind tunnel investigation of a 21 percent scale powered model of a prototype advanced...
Cover title."July 1962."Aerodynamics, aircraft; Aircraft.Includes bibliographical references.Mode of...
Modern rotorcrafts are subjected to some of the most complex flow behaviors ever encountered by the ...
A wind-tunnel investigation was conducted to determine the effects of the main-rotor wake on the aer...
The problem of rotor-fuselage aerodynamic interaction has to be considered in industry applications ...
Longitudinal aerodynamic characteristics of two full-scale helicopter fuselage model
An investigation was conducted in the Langley full-scale tunnel to determine the drag characteristic...
Experimental data are presented for the parasite drag of various helicopter fuselage components, suc...
The present paper describes results of wind tunnel experiments obtained during a research programme ...
Experimental aerodynamic investigations remain the subject of interest in rotorcraft community since...
An investigation has been conducted in the Langley full-scale tunnel to determine the parasite drag ...
Wind-tunnel tests of a heavy-class helicopter model were carried out to evaluate the effectiveness o...
Results of a wind tunnel test campaign to assess technologies for improvement of helicopter fuselage...
Rough conventional, smooth conventional, and laminar-flow or low-drag sections were tested. The item...
An investigation was made in the Langley V/STOL tunnel to determine rotor induced effects on a 1/4-s...
An exploratory wind tunnel investigation of a 21 percent scale powered model of a prototype advanced...
Cover title."July 1962."Aerodynamics, aircraft; Aircraft.Includes bibliographical references.Mode of...
Modern rotorcrafts are subjected to some of the most complex flow behaviors ever encountered by the ...
A wind-tunnel investigation was conducted to determine the effects of the main-rotor wake on the aer...
The problem of rotor-fuselage aerodynamic interaction has to be considered in industry applications ...