PPRuNe Forums - View Single Post - Max perf. take off and Steep landings...
View Single Post
Old 26th November 2007 | 14:05
  #21 (permalink)  
Shawn Coyle
 
Joined: Dec 2001
Posts: 1,835
Likes: 3
From: Philadelphia PA
Topendtorque:

One minor point - the speed for maximum range in a turbine helicopter cannot be determined in the manner you describe due to improved specific fuel consumption at higher power settings. For a turbine, fuel flow vs. airspeed is needed. To be really accurate in determining best range airspeed for both piston and turbine machines, you should use a graph of fuel flow vs. Airspeed.
Several textbooks make this mistake (but not mine!)
Shawn Coyle is offline  
Reply