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Enhancing tensile strength of 3D-printed wood-PLA composites via a particle swarm optimization framework. [PDF]

open access: yesPLoS One
Bhattacharjee B   +7 more
europepmc   +1 more source

Additive Manufacturing of Nanoscale Multimaterial Voxels Via Meniscus-Confined Electrodeposition. [PDF]

open access: yesACS Nano
Sprengel S   +12 more
europepmc   +1 more source
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Advanced Rocket Nozzles

Journal of Propulsion and Power, 1998
Several nozzle concepts that promise a gain in performance over existing conventional nozzles are discussed in this paper. It is shown that signie cant performance gains result from the adaptation of the exhaust e ow to the ambient pressure. Special attention is then given to altitude-adaptive nozzle concepts, which have recently received new interest ...
Hagemann, G.   +3 more
openaire   +3 more sources

Nozzles: Nozzle-less Devices Defined

Journal of the American Rocket Society, 1945
This is a complicated, but exact way of saying that any channel (converge n t divergent, straight or convergentdivergent) through which fluids expand to convert their heat or pressure energy into velocity in a given direction is a nozzle. Since the mass of gas is given a velocity at the expense of its heat or pressure energy, it is seen that the heat ...
openaire   +1 more source

Nozzle Performance Modeling

AIAA Journal, 2002
A polytropic analytical equation system for the internal e ow of nozzles and ducts has been developed by a solution to the combined friction/area change compressible e ow equations. Validation of the system is sought through comparison with experimental data and numerical simulations using FLUENT in the prediction of the performances of two ...
E. A. Wilson, D. Adler, P. Bar-Yoseph
openaire   +1 more source

Flow phenomena in advanced rocket nozzles - The plug nozzle

34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 1998
In recent years, plug nozzles have gained a renewed interest in space business. In principle, this nozzle concept offers a continuous altitude adaptation up to its design pressure ratio. But, the flow adaptation achieved with this advanced rocket nozzle concept induces shocks and expansion waves resulting in exit profiles far away from idealized one ...
Hagemann, G., Immich, H., Terhardt, M.
openaire   +2 more sources

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