uncleflo
Registered since September 28th, 2017
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Tag selected: nozzle.
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Waterproof Rubber Adhesive Repair Tape – SugarDays
Saved by uncleflo on December 19th, 2019.
You can fix almost anything with it. Patch large holes, cracks and gaps. Wide range of applications: With the repair tape, you can immediately seal a spot of water, air and moisture, creating a super-strong, flexible and waterproof shelter. Multipurpose: From the unique design of a thick, flexible, rubberized back, the repair tape can be suitable for any shape or any object. Suitable: Hot / Cold / Wet / Dry / Under Water Temperature resistant: from -21 ℃ to 93 ℃; SPECIFICATION: UV-resistant, environmentally friendly & VOC-free; Color: black, white; Size: 10x152cm / 20x152cm. PACKAGE INCLUDES: 1*Waterproof Rubber Adhesive Repair Tape
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Jet Engine PBS TJ100 - PBS
Saved by uncleflo on August 26th, 2019.
Its advantage is its compact design, low weight with a thrust of up to 1,300 N, and low fuel consumption in the given power category. The generator output is 750 W. One of the PBS TJ100 engine versions enables landing on water. The PBS TJ100 engine is a single-shaft jet engine consisting of a radial compressor, radial and axial diffuser, annular combustion chamber, axial turbine and a fixed outlet nozzle. The PBS TJ100 jet engine was developed for UAVs, missiles, light sport aircraft and gliders with an additional engine. We have delivered hundreds of our jet engines for manned experimental aircrafts and unmanned aircrafts all around the world.
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Rocket Nozzle Flow Analysis on Solidworks - YouTube
Saved by uncleflo on January 18th, 2019.
Rocket Nozzle Flow Analysis on Solidworks, a Youtube movie on how to demonstrate this, using Solidworks. Very educating.
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Interactive Nozzle Simulator
Saved by uncleflo on September 2nd, 2014.
With this software you can investigate how a turbojet or rocket nozzle produces thrust by changing the values of different factors that affect thrust. By changing the shape of the nozzle and the flow conditions upstream and downstream, you can control both the amount of gas that passes through the nozzle and the exit velocity. There is another version of this program that has been modified for rocket nozzles. With the rocket version, you can specify a wider variety of propellant combinations.
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Nozzle Design
Saved by uncleflo on September 2nd, 2014.
A rocket engine uses a nozzle to accelerate hot exhaust to produce thrust as described by Newton's third law of motion. The amount of thrust produced by the engine depends on the mass flow rate through the engine, the exit velocity of the flow, and the pressure at the exit of the engine. The value of these three flow variables are all determined by the rocket nozzle design.
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Air-augmented rocket - Wikipedia, the free encyclopedia
Saved by uncleflo on September 2nd, 2014.
Air-augmented rockets (also known as rocket-ejector, ramrocket, ducted rocket, integral rocket/ramjets, or ejector ramjets) use the supersonic exhaust of some kind of rocket engine to further compress air collected by ram effect during flight to use as additional working mass, leading to greater effective thrust for any given amount of fuel than either the rocket or a ramjet alone. It represents a hybrid class of rocket/ramjet engines, similar to a ramjet, but able to give useful thrust from zero speed, and is also able in some cases to operate outside the atmosphere, with fuel efficiency not worse than both a comparable ramjet or rocket at every point.
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nptelhrd - YouTube
Saved by uncleflo on July 16th, 2014.
This channel provides technical lectures from seven Indian Institutes of Technology (IITs) and Indian Institute of Science (IISc), Bangalore. Please visit the NPTEL Channel List below to view the complete list of courses. (24 Channels)
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NPTEL Principles of Rocket Propulsion
Saved by uncleflo on July 16th, 2014.
A video course shall consist of 40 or more lectures with 1 hour duration per lecture.
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