Calculating Helicopter Downwash Force on a House Roof at 700ft?

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Calculating the downwash force exerted by a helicopter hovering at 700 feet involves numerous variables, including helicopter type, gross weight, altitude, and temperature. Basic momentum theory, which relates to Bernoulli's principle, serves as a foundational approach for these calculations. However, momentum theory is limited in determining induced velocity at specific distances below the rotor, making it challenging to apply directly at 700 feet. For accurate assessments, fluid dynamics simulations or field measurements are recommended due to the complexity of the factors involved. Ultimately, precise calculations require a comprehensive understanding of both theoretical and practical aspects of helicopter aerodynamics.
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Does anyone know how to calculate how much downwards force a helicopter would exert on the roof of a house if it hovered over it at 700ft?

Thanks
 
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Depends, depends, depends.

There are way too many variables that need to be nailed down. Helicopter type. Gross weight. Altitude. Temperature.
 
assume that we have all the parameters, which theory will be used for the calculation?
 
Basic momentum theory in a hover which ties into Bernoulli would be the place to start. Essentially it is calculating the change in momentum of a column of air equivalent in area to the rotor disk.

http://www.public.iastate.edu/~aero442/unit2.pdf
 
apply bernoulli.
basically its the same problem as the old trick. would your truck go light if all the birds inside it took flight at the same time.
and 700 ft a lot of distance
 
Momentum theory is very good to calculate the induced velocity at rotor dics as well as at distance very below the rotor. Unforturnately, it does not have any information for determining the induced velocity at these points which are between the rotor dics and infinite distance, for example at 3 or 4 radiaus below the rotor.
 
Hoangthien said:
Momentum theory is very good to calculate the induced velocity at rotor dics as well as at distance very below the rotor. Unforturnately, it does not have any information for determining the induced velocity at these points which are between the rotor dics and infinite distance, for example at 3 or 4 radiaus below the rotor.
That is very true. Usually something along these lines would be calculated via fluid dynamics package or simply measured in the field. There are so many things that could have an effect on the outcome.
 
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