Author: Martin Hollmann
Publisher: Aircraft Designs Incorporated
ISBN: 9781893639058
Category : Technology & Engineering
Languages : en
Pages : 111
Book Description
Modern Propeller and Duct Design
Author: Martin Hollmann
Publisher: Aircraft Designs Incorporated
ISBN: 9781893639058
Category : Technology & Engineering
Languages : en
Pages : 111
Book Description
Publisher: Aircraft Designs Incorporated
ISBN: 9781893639058
Category : Technology & Engineering
Languages : en
Pages : 111
Book Description
Modern Propeller and Duct Design
Author: Martin Hollmann
Publisher:
ISBN:
Category :
Languages : en
Pages : 111
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 111
Book Description
Ducted Fan Design: Volume 1 - Propulsion Physics and Design of Fans and Long-Chord Ducts
Author: Marc de Piolenc
Publisher: Lulu.com
ISBN: 0359104908
Category :
Languages : en
Pages : 182
Book Description
Publisher: Lulu.com
ISBN: 0359104908
Category :
Languages : en
Pages : 182
Book Description
Aerodynamic Design and Analysis of Propellers for Mini-remotely Piloted Air Vehicles: Ducted propellers
Author: Henry V. Borst
Publisher:
ISBN:
Category : Drone aircraft
Languages : en
Pages : 158
Book Description
Publisher:
ISBN:
Category : Drone aircraft
Languages : en
Pages : 158
Book Description
Modern Propeller and Duct Design
Author: Martin Hollmann
Publisher: Aircraft Designs Incorporated
ISBN: 9781893639058
Category : Technology & Engineering
Languages : en
Pages : 111
Book Description
Publisher: Aircraft Designs Incorporated
ISBN: 9781893639058
Category : Technology & Engineering
Languages : en
Pages : 111
Book Description
A Procedure for Design of Ducts to Reduce Propeller Cavitation and Vibrations
Author: Jui-kung Chʻen
Publisher:
ISBN:
Category : Propellers
Languages : en
Pages : 318
Book Description
Publisher:
ISBN:
Category : Propellers
Languages : en
Pages : 318
Book Description
Numerically-based Ducted Propeller Design Using Vortex Lattice Lifting Line Theory
Author: John M. Stubblefield
Publisher:
ISBN:
Category :
Languages : en
Pages : 74
Book Description
This thesis used vortex lattice lifting line theory to model an axisymmetrical-ducted propeller with no gap between the duct and the propeller. The theory required to model the duct and its interaction with the propeller were discussed and implemented in Open-source Propeller Design and Analysis Program (OpenProp). Two routines for determining the optimum circulation distribution were considered, and a method based on calculus of variations was selected. The results of this model were compared with the MIT Propeller Lifting Line Program (PLL) output for the purpose of validation. Ducted propellers are prevalent in modem marine propulsion systems, and the application of this technology continues to expand. The theory associated with ducted propellers applies to a wide-range of devices which include azimuth thrusters, pumpjets, and tidal turbines. Regardless of the application, engineers need tools such as OpenProp to design these devices for their expected operating conditions. OpenProp is an open source MATLAB®-based suite of propeller numerical design tools. Previously, the program only designed open propellers. The code developed in this thesis extended OpenProp's capability to be able to design a propeller within an axisymmetrical duct.
Publisher:
ISBN:
Category :
Languages : en
Pages : 74
Book Description
This thesis used vortex lattice lifting line theory to model an axisymmetrical-ducted propeller with no gap between the duct and the propeller. The theory required to model the duct and its interaction with the propeller were discussed and implemented in Open-source Propeller Design and Analysis Program (OpenProp). Two routines for determining the optimum circulation distribution were considered, and a method based on calculus of variations was selected. The results of this model were compared with the MIT Propeller Lifting Line Program (PLL) output for the purpose of validation. Ducted propellers are prevalent in modem marine propulsion systems, and the application of this technology continues to expand. The theory associated with ducted propellers applies to a wide-range of devices which include azimuth thrusters, pumpjets, and tidal turbines. Regardless of the application, engineers need tools such as OpenProp to design these devices for their expected operating conditions. OpenProp is an open source MATLAB®-based suite of propeller numerical design tools. Previously, the program only designed open propellers. The code developed in this thesis extended OpenProp's capability to be able to design a propeller within an axisymmetrical duct.
Marine Propellers and Propulsion
Author: John Carlton
Publisher: Butterworth-Heinemann
ISBN: 0080971237
Category : Technology & Engineering
Languages : en
Pages : 539
Book Description
The early development of the screw propeller. Propeller geometry. The propeller environment. The ship wake field, propeller performance characteristics.
Publisher: Butterworth-Heinemann
ISBN: 0080971237
Category : Technology & Engineering
Languages : en
Pages : 539
Book Description
The early development of the screw propeller. Propeller geometry. The propeller environment. The ship wake field, propeller performance characteristics.
Aircraft Propeller Design
Author: Fred Ernest Weick
Publisher:
ISBN:
Category : Transportation
Languages : en
Pages : 320
Book Description
En lærebog om flypropeller.
Publisher:
ISBN:
Category : Transportation
Languages : en
Pages : 320
Book Description
En lærebog om flypropeller.
An Experimental Verification of a Design Method for Ducted Propellers
Author: Gilbert Dyne
Publisher:
ISBN:
Category : Propellers
Languages : en
Pages : 26
Book Description
Starting from known values of total thrust, number of revolutions, duct vorticity etc. the method determines ducted propeller efficiency, duct thrust, shape of the duct and the propeller etc. The distribution of blade circulation is arbitrary and the number of propeller blades finite. To simplify the calculations a combination of the method of singularities and the momentum theorem is used. (Author).
Publisher:
ISBN:
Category : Propellers
Languages : en
Pages : 26
Book Description
Starting from known values of total thrust, number of revolutions, duct vorticity etc. the method determines ducted propeller efficiency, duct thrust, shape of the duct and the propeller etc. The distribution of blade circulation is arbitrary and the number of propeller blades finite. To simplify the calculations a combination of the method of singularities and the momentum theorem is used. (Author).