B260
OTHER:
Helicopters - Rotor Disk & Horsepower Specifications:![]()
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Hover Flight for single rotor applications is working. Calculations for multiple rotors have some errors. |
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Vertical Flight and Forward Flight have some errors also |
These calculations are from 'Momentum Theory' and 'Combined Momentum and Blade Element Theory with Empirical Corrections' from chapter 1 of Helicopter Performance, Stability and Control by Raymond W. Prouty. Additions have been made for helicopters with multiple rotors.
These pages are in support of the Homebuilt helicopter community. If anyone wishes to correct an input value on an existing helicopter (some of which have had to be assumed) or question a calculated value, please e-mail me so these pages can be made as accurate as possible.
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Input;
Not Currently in UseIf this is an initial request, then you must give your e-mail address so that you may be advised of the web page address of your specifications
If this is a revision to a previous input, you may wish to print your current web pages before they are changed.
Input of Helicopter Specifications
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For calculated data on an existing helicopter: (& SynchroLite); click on that helicopter. Other light helicopters can be added if there is a request.
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Ultralights: |
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~ cont. ~ |
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1 seat: |
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~ cont. ~ |
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2 seats: |
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Large: |
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~ The data on the above helicopters contains errors. ~
The latest additions contains horsepower calculation errors in;
Earlier helicopters have even more errors.
For calculated data based on your previously submitted input:
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OTHER:
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Database Calculations |
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Last Revised: October 24, 2002