Add to ORKGLongitudinal aerodynamic characteristics of two full-scale helicopter fuselage model
Experimental data are presented for the parasite drag of various helicopter fuselage components, suc...
As part of the general helicopter research program being undertaken by the National Advisory Committ...
(Maximum 200 words) A wind-tunnel investigation was conducted to determine two-dimensional aerodyna...
Wind tunnel investigation of drag and static stability characteristics of four helicopter fuselage m...
An investigation was conducted in the Langley full-scale tunnel to determine the drag characteristic...
The present paper describes results of wind tunnel experiments obtained during a research programme ...
Wind-tunnel tests of a heavy-class helicopter model were carried out to evaluate the effectiveness o...
An investigation was made in the Langley V/STOL tunnel to determine rotor induced effects on a 1/4-s...
Cover title."July 1962."Aerodynamics, aircraft; Aircraft.Includes bibliographical references.Mode of...
An exploratory wind tunnel investigation of a 21 percent scale powered model of a prototype advanced...
A wind-tunnel investigation was conducted to determine 2-D aerodynamic characteristics of nine polyg...
An investigation has been conducted in the Langley full-scale tunnel to determine the parasite drag ...
The problem of rotor-fuselage aerodynamic interaction has to be considered in industry applications ...
Results of a wind tunnel test campaign to assess technologies for improvement of helicopter fuselage...
In this paper, wind tunnel experiments are combined with Computational Fluid Dynamics (CFD) aiming ...
Experimental data are presented for the parasite drag of various helicopter fuselage components, suc...
As part of the general helicopter research program being undertaken by the National Advisory Committ...
(Maximum 200 words) A wind-tunnel investigation was conducted to determine two-dimensional aerodyna...
Wind tunnel investigation of drag and static stability characteristics of four helicopter fuselage m...
An investigation was conducted in the Langley full-scale tunnel to determine the drag characteristic...
The present paper describes results of wind tunnel experiments obtained during a research programme ...
Wind-tunnel tests of a heavy-class helicopter model were carried out to evaluate the effectiveness o...
An investigation was made in the Langley V/STOL tunnel to determine rotor induced effects on a 1/4-s...
Cover title."July 1962."Aerodynamics, aircraft; Aircraft.Includes bibliographical references.Mode of...
An exploratory wind tunnel investigation of a 21 percent scale powered model of a prototype advanced...
A wind-tunnel investigation was conducted to determine 2-D aerodynamic characteristics of nine polyg...
An investigation has been conducted in the Langley full-scale tunnel to determine the parasite drag ...
The problem of rotor-fuselage aerodynamic interaction has to be considered in industry applications ...
Results of a wind tunnel test campaign to assess technologies for improvement of helicopter fuselage...
In this paper, wind tunnel experiments are combined with Computational Fluid Dynamics (CFD) aiming ...
Experimental data are presented for the parasite drag of various helicopter fuselage components, suc...
As part of the general helicopter research program being undertaken by the National Advisory Committ...
(Maximum 200 words) A wind-tunnel investigation was conducted to determine two-dimensional aerodyna...