Recent content by spiveycool
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Are Electric Superchargers Worth the Energy Storage Concerns?
densifier I am working on a fuel/O2 gas powered turbo system. Any thoughts?- spiveycool
- Post #5
- Forum: Mechanical Engineering
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Effects of temperature/pressure on power output
How much power would be produced when using an independently powered supply of 100 pound/min air at 3bar/40F air on a 6.2L GM LS V8. Excess air will be vented to atmosphere with relief valves to stabilize the air flow to the throttle valve. What are the factors need to be considered...- spiveycool
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- Effects Output Power Power output
- Replies: 1
- Forum: Mechanical Engineering
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Exact Purpose of Hemispherical Heads?
Yes. The hemi head design allows a much better port to valve design and a permits a central spark plug placement in the cylinder. This permits a very straight port to valve design This design has dominated NHRA top fuel drag racing for the last 50 years.- spiveycool
- Post #15
- Forum: Mechanical Engineering
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Liquid rocket gas generator question
NASA made a steam generator for the Stennis center that consisted of the injector head of a flight engine installed in a straight pipe with water injection jets at the bottom to inject water against the gas flow to make steam. I want to make a similar setup to make 35 lb/sec@ 1700F steam. I...- spiveycool
- Post #5
- Forum: Aerospace Engineering
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Liquid rocket gas generator question
Engine is copy of project motor described in ROCKETLABS book- How to design,build and test small rocket engines. I intend to use it to drive a GARRETT turbo and rework or cast and machine new exhaust side housing to suit application.Turbochargers are designed to operate with high volume/low...- spiveycool
- Post #3
- Forum: Aerospace Engineering
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Liquid rocket gas generator question
I am building a liquid fueled rocket engine driven gas generator. I plan to use gasoline for fuel and oxygen gas at a rate of .022lb/sec and O2 at .055lb/sec The chamber is 2.15 in long 1.15 in id with a .238 nozzle. The chamber pressure should be 300 psi with a thrust of 20 pounds. I calculate...- spiveycool
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- Gas Generator Liquid Rocket
- Replies: 5
- Forum: Aerospace Engineering