Harnessing DDT
Posted: Wed Mar 25, 2009 3:28 am
Well this project is mainly the theoretical, inspire higher thinking type. That aside, action may be taken depending on the results.
The topic is DDT. Some of you may be familiar with it, some not. The general statement is that DDT occurs when the flame front reaches a supersonic speed.
DDT
The wiki states that it can create a gigantic pressure spike that can destroy the chamber.
If one could build a strong enough chamber, surely the immense increase in pressure could give an extremely powerful shot.
Factors that increase the likelihood of DDT:
-Rapidly burning fuels (hydrogen, acetylene)
-Presence of oxidizer (oxygen)
-Longer, thinner chamber
-Higher mixes
If these factors could be combined to produce DDT on a reliable basis, could we expect much more power?
So essentially:
If one was to build a (very) small launcher what kind of reinforcement would be required to harness the DDT blast- A.K.A. how much more powerful would a (mach) flame front be than say one of 1/2 (mach). From what I've been led to see it would not have a ratio directly proportional to the speed above mach.
Any input?
The topic is DDT. Some of you may be familiar with it, some not. The general statement is that DDT occurs when the flame front reaches a supersonic speed.
DDT
The wiki states that it can create a gigantic pressure spike that can destroy the chamber.
If one could build a strong enough chamber, surely the immense increase in pressure could give an extremely powerful shot.
Factors that increase the likelihood of DDT:
-Rapidly burning fuels (hydrogen, acetylene)
-Presence of oxidizer (oxygen)
-Longer, thinner chamber
-Higher mixes
If these factors could be combined to produce DDT on a reliable basis, could we expect much more power?
So essentially:
If one was to build a (very) small launcher what kind of reinforcement would be required to harness the DDT blast- A.K.A. how much more powerful would a (mach) flame front be than say one of 1/2 (mach). From what I've been led to see it would not have a ratio directly proportional to the speed above mach.
Any input?