Includes bibliographical references (pages 37-38)The United States Army Aviation Engineering Flight Activity conducted an airworthiness and flight characteristic evaluation of the improved main rotor blade manufactured by Kaman Aerospace Corporation which was installed on the YAH-lR helicopter. Both the standard Bell 8540 and Kaman K747 rotor blades were evaluated for hover performance. The results of the B540 blades were used as a baseline for comparison to the K747 results. Both sets of hover performance data were analyzed using techniques based upon established statistical and probability theories. The results of these analysis and hypothesis testing were the rejection of the contractors claim of a 8.7% improvement in hover performance
Instrument-flying trials have been conducted in a single-rotor helicopter to determine the adequacy ...
Measurements of the static-thrust performance of six sets of rotor blades mounted on a helicopter fu...
Rotor hover-performance data from a 1/6-scale helicopter rotor are analyzed and the data sets compar...
An investigation was conducted in the NASA Langley Transonic Dynamics Tunnel to evaluate an advanced...
A flight investigation produced data on performance and rotor loads for a teetering rotor, AH-1G hel...
Two rotor systems for the UH-1 helicopter were tested in hover and forward flight. The baseline syst...
Flight test measurements of the performance of the UH-60 Black Hawk helicopter with both standard an...
A cooperative study was performed to investigate the handling quality effects from reduced flight co...
Four cases were selected for comparison with theoretical predictions using stability data obtained d...
An investigation was conducted in the Langley Transonic Dynamics Tunnel to evaluate differences betw...
Flight data were obtained with an instrumented AH-16 helicopter having uninstrumented, standard main...
Performance of a 27 percent scale model rotor designed for the AH-64 helicopter (alternate rotor) wa...
This paper presents the results from an experimental study of the aerodynamic performance and effici...
In order to facilitate solutions of the general problem of helicopter selection, the aerodynamic per...
Charts showing the rotor profile drag-lift ratio are presented for a helicopter rotor operating in f...
Instrument-flying trials have been conducted in a single-rotor helicopter to determine the adequacy ...
Measurements of the static-thrust performance of six sets of rotor blades mounted on a helicopter fu...
Rotor hover-performance data from a 1/6-scale helicopter rotor are analyzed and the data sets compar...
An investigation was conducted in the NASA Langley Transonic Dynamics Tunnel to evaluate an advanced...
A flight investigation produced data on performance and rotor loads for a teetering rotor, AH-1G hel...
Two rotor systems for the UH-1 helicopter were tested in hover and forward flight. The baseline syst...
Flight test measurements of the performance of the UH-60 Black Hawk helicopter with both standard an...
A cooperative study was performed to investigate the handling quality effects from reduced flight co...
Four cases were selected for comparison with theoretical predictions using stability data obtained d...
An investigation was conducted in the Langley Transonic Dynamics Tunnel to evaluate differences betw...
Flight data were obtained with an instrumented AH-16 helicopter having uninstrumented, standard main...
Performance of a 27 percent scale model rotor designed for the AH-64 helicopter (alternate rotor) wa...
This paper presents the results from an experimental study of the aerodynamic performance and effici...
In order to facilitate solutions of the general problem of helicopter selection, the aerodynamic per...
Charts showing the rotor profile drag-lift ratio are presented for a helicopter rotor operating in f...
Instrument-flying trials have been conducted in a single-rotor helicopter to determine the adequacy ...
Measurements of the static-thrust performance of six sets of rotor blades mounted on a helicopter fu...
Rotor hover-performance data from a 1/6-scale helicopter rotor are analyzed and the data sets compar...