PPRuNe Forums - View Single Post - Multiple rotor vs single rotor efficiency
Old 15th January 2008 | 21:41
  #36 (permalink)  
Graviman
 
Joined: Nov 2004
Posts: 1,334
Likes: 0
From: Cambridgeshire, UK
For what application, Dave?

Much of the time i use software packages developed specifically to solve Finite Element problems or CAD problems. If i am trying to model something in more detail i have been known to write iterative code in Excel. I have written powertrain performance simulations in Pascal and test data processing in Fortran. I have even programmed 4 bit computers in machine code.

But my point is that a control system does not need to be complicated. When my old man was a rocket scientist at Hawker Siddely it was often done using gyros and analogue circuits. In fact the only real advantage of digital is very complex circuitry with no noise. As i say Lockheed did it mechanically.

But there are folk who specialise in this. It would be unrealistic to expect an experimental / homebuilt to perform as well as an OEM machine. If you used the config to get the same handling, the payload/machine ratio would suffer for both cost and weight.

Helicopter design is all about extending the margins...

Last edited by Graviman; 15th January 2008 at 22:01.
Graviman is offline  
Reply