Dan asked:

> Does anyone have any figures on how much difference 

> changing the pitch of the prop makes in cruise and climb?

 

My observation on cruise speed and pitch with the C-85:

 

All observations at 2400 rpm

7146   100 mph       climb prop

7148   104 mph       normal prop (per Ed and John)

7150   108 mph       cruise prop (per Ed and John)

7150   112 mph       theoretical - several heavy or draggy Coupes have shown
they can only make it to 90 mph with miserable climb using this pitch.

 

These correspond pretty well between my observations/measurements and Paul
Prentice's information duplicated below.

 

Sorry that I don't have good climb tables.

 

Ed Burkhead

http://edburkhead.com/Ercoupe/index.htm           East Peoria, Illinois

ed -at- edburk???head.??com                      (remove the ? marks and
change -at- to @)

 

Engine/Propeller efficiency

Paul Prentice published tables in his 1991 book "Fly About Adventures and
the Ercoupe." His tables have checked out pretty well, from my experience
with measured speeds during in-flight observations. Ed Burkhead
  
The following material is used by permission of the author and copyright
holder, Paul Prentice.  Paul may be contacted at [EMAIL PROTECTED] to request
permission for any other use. All rights reserved.
 


For each engine, these are at the "recommended cruising RPM according to the
"Operators Manual" by Teledyne Continental Motors Form X30012 FAA approved
Dec. 1980.
  
All numbers @ 5.1 degrees Celsius @ 5,000 feet.
C-75 @ RPM=2275    prop=CL7349    IAS=102    TAS=110
                   prop=ST7351    IAS=106    TAS=114
                   prop=CR7353    IAS=111    TAS=119
  
C-90 @ RPM=2350    prop=CL7150    IAS=106    TAS=114
                   prop=ST7152    IAS=110    TAS=118
                   prop=CR7153    IAS=114    TAS=123

C-85 @ RPM=2400    prop=CL7148    IAS=104    TAS=112
                   prop=ST7150    IAS=108    TAS=116
                   prop=CR7152    IAS=112    TAS=121

O-200 @ RPM=2500   prop=CL6948    IAS=103    TAS=111
                   prop=ST6950    IAS=108    TAS=116
                   prop=CR6952    IAS=112    TAS=121
  
For comparison:  The C-85 with a 50 inch pitch prop.  The 50 inch pitch
means it would theoretically travel 50 inches forward during one turn.
  
113.6 miles/hour = (50 inches * 2400 rev/min * 60 min/hour ) / (12
inches/foot) / (5280 feet/mile)
  
  
  
ENGINE  PROP  COUPE    AVG     CRUISE  TIAS    TAS   MAX   IAS     TAS
 TYPE   SIZE  MODEL EFFICIENCY  RPM   SEA LVL 5000'  RPM  SEA LVL 5000'
  
C-75    7351   C-D      97      2275   106     114   2275  106     114
  
C-85    7150  CD-to-G   95      2400   108     116   2575  116     125
  
C-90    7152  F1-F1A    95      2350   110     118   2475  116     125
  
C-90    7153  A2-A2A    97      2350   114     123   2475  120     129
  
O-200   6950   D-G      91      2500   108     116   2750  118     127
  
  These are the best table I've seen.

 

 

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