Investigation Of The Aerodynamic Characteristics Of A Model Wing Propeller Combination And Of The Wing And Propeller Separately At Angles Of Attack Up To 90 PDF Download

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Investigation of the Aerodynamic Characteristics of a Model Wing-propeller Combination and of the Wing and Propeller Separately at Angles of Attack Up to 90°

Investigation of the Aerodynamic Characteristics of a Model Wing-propeller Combination and of the Wing and Propeller Separately at Angles of Attack Up to 90°
Author: John W. Draper
Publisher:
Total Pages: 82
Release: 1954
Genre: Aerodynamics
ISBN:

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This report presents the results of an investigation conducted in the Langley 300 mph 7- 10-foot wind tunnel for the purpose of determining the aerodynamic characteristics of a model wing-propeller combination, and of the wing and propeller separately at angles of attack up to 90 degrees. The tests covered thrust coefficients corresponding to free-stream velocities from zero forward speed to the normal range of cruising speeds. The results indicate that increasing the thrust coefficient increases the angle of attack for maximum lift and greatly diminishes the usual reduction in lift above the angle of attack for maximum lift.


Charts for Estimating Rotor-blade Flapping Motion of High-performance Helicopters

Charts for Estimating Rotor-blade Flapping Motion of High-performance Helicopters
Author: Robert J. Tapscott
Publisher:
Total Pages: 692
Release: 1956
Genre: Charts, diagrams, etc
ISBN:

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Theoretically derived charts showing steady-state and first- and second-harmonic flapping coefficients are presented for helicopter rotors having hinged rectangular blades with a linear twist of 0, -8, and -16 degrees. The charts, showing the rotor flapping coefficients for combinations of inflow ratio and blade pitch angle, are presented for tip-speed ratios ranging from 0.05 to 0.50.


Wind-tunnel Investigation of Longitudinal Aerodynamic Characteristics of Three Propeller-driven VTOL Configurations in the Transition Speed Range, Including Effects of Ground Proximity

Wind-tunnel Investigation of Longitudinal Aerodynamic Characteristics of Three Propeller-driven VTOL Configurations in the Transition Speed Range, Including Effects of Ground Proximity
Author: Richard E. Kuhn
Publisher:
Total Pages: 134
Release: 1960
Genre: Aerodynamics
ISBN:

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Technical Note

Technical Note
Author:
Publisher:
Total Pages: 460
Release: 1955
Genre: Aeronautics
ISBN:

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