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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

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 ...
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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

The TICTOP nozzle: a new nozzle contouring concept

CEAS Space Journal, 2016
Currently, mainly two types of nozzle contouring methods are applied in space propulsion: the truncated ideal contour (TIC) and the thrust-optimized parabola (TOP). This article presents a new nozzle contouring method called TICTOP, combining elements of TIC and TOP design.
Manuel Frey   +2 more
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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

Supersonic Annular Nozzles

Journal of Spacecraft and Rockets, 1971
An analytical method is presented for the design of axisymmetric annular nozzles to yield uniform and axial flow. Computed results are used to display typical matched inner and outer contours, the effects of major initial flow variables, and the resulting wall forces.
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The Effect of Nozzles and Nozzle Loadings on Shell Buckling

Volume 3: Design and Analysis, 2015
This paper investigates the effect of nozzles and nozzle loadings on the overall buckling capacity of a vessel subject to external pressure designed to ASME VIII Div 1. ASME VIII Div 1 provides a well-established design-by-rule (DBR) approach for vessels subject to external pressure, but this takes no consideration for the presence of ...
Edward Clarke, Robert Frith
openaire   +1 more source

Aggregate Breakup in a Contracting Nozzle

Langmuir, 2009
The breakup of dense aggregates in an extensional flow was investigated experimentally. The flow was realized by pumping the suspension containing the aggregates through a contracting nozzle. Variation of the cluster mass distribution during the breakage process was measured by small-angle light scattering.
M. Soos   +3 more
openaire   +4 more sources

Model tests with nozzles and steering nozzles for trawlers1

International Shipbuilding Progress, 1965
With a trawler model several nozzle propeller arrangements were tested in still water both free running and when trawling. Special attention was paid to turning ability and rudder head torques to be expected with steering nozzles.
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Truncated Perfect Nozzles in Optimum Nozzle Design

ARS Journal, 1961
A graphical technique for selecting optimum nozzle contours from a family of truncated perfect nozzles is presented which permits simultaneous consideration of various types of optima. This procedure includes the effects of friction, as well as the thermodynamic properties of the reacting gas.
J. H. AHLBERG   +3 more
openaire   +1 more source

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