Subject: Tip Speed and prop efficiency.
From: Paul
Date: 2/20/2000, 9:18 AM

Ken Powell wrote:

Paul,
I have been following the discussion of prop tip speeds but none of
the charts presented an answer that I could see to the following
question?  (I am a programmer and I am sometimes mathamatically
challenged!)
-- On a 200 MPH airplane (RVx), at what propeller RPM do the tips
enter the high drag transonic speed that we need to avoid?
1.  for a 68" prop
2.  for a 70" prop
3.  for a 72" prop
I also noticed last week that one of the charts seemed to present
evidence that prop diameter changes of this small magnitude were not
significant, but the results of real world tests seem to indicate
that they do.  What is the 'real' story here?
Please give me some guidance here; there doesn't seem to be an easy
answer.  I know that 'thinning' the tips will allow higher RPM, but
I would like the issue addressed for standard wood props like we
would buy from most of the prop makers.
Thanks,
Ken Powell

Here are the numbers Ken.

According to the data Vance gave me there will be a slight advantage
in static thrust for the 72 verses the 68 inch prop but little or no 
advantage at top speed.

Just to cloud the issue further.. for most aircraft engines, for the same tip mach
number, you will get slightly more HP with the smaller prop because the engine
is running faster.

BTW a Cessna 150 takes off pretty good with a fixed pitch prop as the ratio
of top speed to takeoff speed is not much so a fine pitch prop can be 
chosen. Ultra lights are in the same category as the takeoff, cruise and stall
speeds are all the same :-) 
 
It is when you are confronted with a wide speed range airplane such as 
a Lancair 360 or an RV that can cruise over 200 MPH  that constant speed 
props show a huge advantage in much faster takeoffs. 

Vance neglected to mention this and I was too stupid to pick up on it. :-)
As I recall Vance used a fixed pitch prop optimized for only 180 MPH in his chart.
If you optimize a fixed pitch prop for 220 MPH the takeoff thrust will
suffer greatly. I still believe the Air Master chart for the Lancair with 
the constant speed prop.

I spoke to Tracy Saylor, owner of the fastest RV6 in the world at 228 MPH, about this
and he said he reduced the fine pitch stop on his constant speed prop so the engine 
could reach 2800 RPM for max power  and it does so within a second of starting to
taking off. 

It takes off in less than three seconds. It all happens so fast it is difficult 
to know exactly when the engine reaches 2800 RPM or to get accurate data with a hand 
held stop watch. I intend to spend the money and put a constant speed prop
on my turbo 13B powered KIS cruiser. As far as I am concerned it is the best
investment in overall aircraft performance and takeoff safety.

Paul Lamar
 
The Aircraft Rotary Engine Newsletter.              Powered by Linux.

http://home.earthlink.net/~rotaryeng/            http://www.linux.org

MACHVDIA.DAT
dia =  68 
  RPM    Tip FPS  Vel FPS    Vel MPH    Mach
  2200      653      716      488       0.70
  2250      668      729      497       0.71
  2300      682      743      506       0.72
  2350      697      756      516       0.74
  2400      712      770      525       0.75
  2450      727      784      534       0.76
  2500      742      798      544       0.78
  2550      757      811      553       0.79
  2600      771      825      563       0.80
  2650      786      839      572       0.82
  2700      801      853      582       0.83
  2750      816      867      591       0.84
  2800      831      881      601       0.86
dia =  69 
  RPM    Tip FPS  Vel FPS    Vel MPH    Mach
  2200      662      724      494       0.71
  2250      677      738      503       0.72
  2300      692      752      513       0.73
  2350      708      766      522       0.75
  2400      723      780      532       0.76
  2450      738      794      541       0.77
  2500      753      808      551       0.79
  2550      768      822      560       0.80
  2600      783      836      570       0.81
  2650      798      850      580       0.83
  2700      813      864      589       0.84
  2750      828      878      599       0.86
  2800      843      893      609       0.87
dia =  70 
  RPM    Tip FPS  Vel FPS    Vel MPH    Mach
  2200      672      733      500       0.71
  2250      687      747      509       0.73
  2300      702      761      519       0.74
  2350      718      775      529       0.76
  2400      733      790      538       0.77
  2450      748      804      548       0.78
  2500      764      818      558       0.80
  2550      779      832      567       0.81
  2600      794      847      577       0.82
  2650      809      861      587       0.84
  2700      825      875      597       0.85
  2750      840      890      607       0.87
  2800      855      904      616       0.88
dia =  71 
  RPM    Tip FPS  Vel FPS    Vel MPH    Mach
  2200      682      742      506       0.72
  2250      697      756      516       0.74
  2300      713      771      525       0.75
  2350      728      785      535       0.76
  2400      744      799      545       0.78
  2450      759      814      555       0.79
  2500      774      828      565       0.81
  2550      790      843      575       0.82
  2600      805      857      584       0.83
  2650      821      872      594       0.85
  2700      836      886      604       0.86
  2750      852      901      614       0.88
  2800      867      916      624       0.89
dia =  72 
  RPM    Tip FPS  Vel FPS    Vel MPH    Mach
  2200      691      751      512       0.73
  2250      707      765      522       0.75
  2300      723      780      532       0.76
  2350      738      794      542       0.77
  2400      754      809      552       0.79
  2450      770      824      562       0.80
  2500      785      838      572       0.82
  2550      801      853      582       0.83
  2600      817      868      592       0.85
  2650      833      883      602       0.86
  2700      848      898      612       0.87
  2750      864      912      622       0.89
  2800      880      927      632       0.90