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The Aerodynamic Design of Supersonic Propellers from Structural Considerations

The Aerodynamic Design of Supersonic Propellers from Structural Considerations PDF Author: Jerome B. Hammack
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 682

Book Description
The aerodynamic design of propellers from considerations of centrifugal force is presented. A solution is obtained for the span wise distribution of cross-sectional area required to attain constant centrifugal stress over most of the blade.

The Aerodynamic Design of Supersonic Propellers from Structural Considerations

The Aerodynamic Design of Supersonic Propellers from Structural Considerations PDF Author: Jerome B. Hammack
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 682

Book Description
The aerodynamic design of propellers from considerations of centrifugal force is presented. A solution is obtained for the span wise distribution of cross-sectional area required to attain constant centrifugal stress over most of the blade.

Technical Note - National Advisory Committee for Aeronautics

Technical Note - National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 554

Book Description


Technical Note

Technical Note PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 506

Book Description


Report

Report PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 620

Book Description


Report - National Advisory Committee for Aeronautics

Report - National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1246

Book Description


Study of the Supersonic Propeller

Study of the Supersonic Propeller PDF Author: Jean Fabri
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 640

Book Description
In this paper a propeller having all sections operating at supersonic speeds is designated a supersonic propeller regardless of flight speed. Analyses assume subsonic flight speeds but very high rotational speeds. A very elementary analysis of the efficiency of a jet-propeller system is presented. A propeller analysis based on conventional vortex blade element theory is presented and reduced to a single point method which leads to an expression for optimum advance ratio in terms of hub-tip diameter ratio and airfoil fineness ratio. An expression for propeller efficiency in terms of advance ratio, hub-tip diameter ratio, and airfoil thickness ratio is also presented. Use is made of theoretical airfoil characteristics at supersonic speeds. A study of blade section interference, blade shock and expansion fields, at supersonic section speeds is presented. An example taken indicates that an efficiency of seventy percent can be obtained with a propeller having a tip Mach number of 2.3.

Annual Report

Annual Report PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 534

Book Description


Applied Mechanics Reviews

Applied Mechanics Reviews PDF Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 1006

Book Description


List of Technical Notes, 1947-1953

List of Technical Notes, 1947-1953 PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 162

Book Description


WADC Technical Note

WADC Technical Note PDF Author: United States. Wright Air Development Division
Publisher:
ISBN:
Category :
Languages : en
Pages : 912

Book Description