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Old 11-23-2005 | 06:04 PM
  #30  
Miniflyer
 
Joined: Dec 2004
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From: Neuburg, GERMANY
Default RE: variable exaust nozzle


ORIGINAL: starwoes



why you'd want a mach+++ exhaust velocity on a model airplane engine is something else beyond me.

Simply because, as you stated yourself, thrust = mass x velocity². Increasing the velocities (into the Mach numbers) increases thrust...
The theory and work involved in creating a variable nozzle going beyond Mach 1 would be outrageous, though...and would have to be preceeded by a nozzle getting it up to 1.0 in the first place.

Be an interesting project...however first i need to get my other projects off the table, which may very well last a few more years at my current rate...

Hank