It is tough to do using all the inputs of RPM, MAP, temperature and altitude. With all that stuff you still need a computer or very complicated chart. I think all you will be able to do is make a very rough guess or maybe get in a situation where you are full throttle and derive a likely manifold pressure by calculation and comparison to other similar airplanes.Can anyone out there tell me what the % power vs. rpm is for an O360-180hp, fixed pitch (72x85) for an RV7A? I would like to check my speeds against Van's spec's but I don't know where 75% & 55% power settings are. I have no MAP indication.
Can anyone out there tell me what the % power vs. rpm is for an O360-180hp, fixed pitch (72x85) for an RV7A? I would like to check my speeds against Van's spec's but I don't know where 75% & 55% power settings are. I have no MAP indication.
Can anyone out there tell me what the % power vs. rpm is for an O360-180hp, fixed pitch (72x85) for an RV7A? I would like to check my speeds against Van's spec's but I don't know where 75% & 55% power settings are. I have no MAP indication.
75% is easy. Climb to 8500' and let it roll at wide open throttle. It is close enough for the comparison and government work.
I've been told that straight & level full power RPM - 10% = 75% power setting.
Also, here is a fairly accurate formula for calculating speed.
RPM X Pitch X .000947 = MPH
Thank you guys for the wealth of information you have provided. Please forgive my rustiness but if my field elevation is 500' and the DA is 1500', does that mean that I need to climb to 9000' agl to reach 8000' DA?
My chart was developed for my use with a fixed pitch climb prop used at high altitudes but it was developed with the use of one of Kevin Horton's power spreadsheets. I think many people should find these very useful as it is much easier to just punch the numbers in your computer than to deal with Lycoming's charts. You could also use his spreadsheet to develop your own chart....The only problem with this chart is that it only goes up to 80% power.
Top speed in a normally aspirated airplane would normally be found at sea level at full power.... So if full throttle at 8000' yields 75% power, what is Van's top speed based on?
Full throttle at sea level at standard temperature. I.E 100% power.Based on the excellent information given, I have another question:
Van's performance specs for RV7-180hp says: 200 mph @ 75% @ 8000' c/s. If 75% pwr is full throttle at 8000', what is Van's top speed of 210 mph based on?