Ref: http://142.26.194.131/aerodynamics1/Multi/Page2.html

A windmilling prop at low idle will actually produce more drag than a stopped 
prop.  However, with the engine turning at a high idle, it will help carry you 
a long ways.  I nursed a Stinson Voyager 8 miles at night from 1700'AGL with 
best power variable from 1400 - 1700 RPM as the remains of the engine beat 
itself to pieces.  That's just above a high idle, but significantly lengthened 
the glide to safely make it to a runway.  

However, your point is well made that a little bit of power makes a huge 
difference in glide.

-Jeff

-- "Orma" <o...@aviation-mechanics.com> wrote:
Hello Net
I have read the responses on glide ratio and see that no one has made the 
real test with the engine off.   Any number that you get with the engine a 
idle is an over estimate.  How much of an over estimate depends on the 
thrust the engine and prop combo put out at your particular idle speed.  My 
KR on it's first flight had the Idle too high and would not stop flying and 
continued to float down a 10,000 foot runway until I cut the engine off. 
I'm saying this yet, I don't recommend power off testing.  Knowing how the 
aircraft controls at minimum controllable airspeed is probably the most 
useful information you can have besides knowing and having a feel for how 
and when your KR will stall.  If I feel that my engine is not reliable, I 
head to the nearest airport.  Along the way I continually look for a safe 
place to land.  I have never considered the question  "If my engine quit how 
far could I go?"  Better to pick a spot to land then to try and fail to make 
it that last mile.
Orma
Southfield, MI
N110LR Tweety, old enough to drink this year
Flying and more flying, to the gathering or bust
http://www.kr-2.aviation-mechanics.com/ 



_______________________________________
Search the KRnet Archives at http://www.maddyhome.com/krsrch/index.jsp
to UNsubscribe from KRnet, send a message to krnet-le...@mylist.net
please see other KRnet info at http://www.krnet.org/info.html


Reply via email to