Possible Origin of the Secondary Stream of Neutral Fluxes at 1 AU

Author(s):  
Peter Wurz
Keyword(s):  
2021 ◽  
Vol 113 ◽  
pp. 106697
Author(s):  
Rui Gu ◽  
Mingbo Sun ◽  
Zun Cai ◽  
Jian Chen ◽  
Peibo Li ◽  
...  

Author(s):  
K-H Lee ◽  
T Setoguchi ◽  
S Matsuo ◽  
H-D Kim

The present study addresses experimental investigations of the near-field flow structures of an underexpanded sonic, dual, coaxial, swirl jet. The swirl stream is discharged from the secondary annular nozzle and the primary inner nozzle provides the underexpanded free jets. The interactions between the secondary swirl and primary underexpanded jets are quantified by a fine pitot impact and static pressure measurements and are visualized using a shadowgraph optical method. The pressure ratios of the secondary swirl and primary underexpanded jets are varied below 7.0. Experiments are conducted to investigate the effects of the secondary swirl stream on the primary underexpanded jets, compared with the secondary stream of no swirl. The results show that the presence of an annular swirl stream causes the Mach disc to move further downstream, with an increased diameter, and remarkably reduces the fluctuations of the impact pressures in the underexpanded sonic dual coaxial jet, compared with the case of the secondary annular stream with no swirl.


1960 ◽  
Vol 82 (1) ◽  
pp. 120-129 ◽  
Author(s):  
H. E. Weber

An analysis for predicting the secondary and primary flows and the thrust coefficient of ejector nozzles is presented. Particular attention is given to the diverging shroud ejector in which the throat of the secondary stream is formed at a small distance down-stream of the primary nozzle exit; i.e., near the plane of the minimum shroud area. The basic assumption in the analysis is that the shroud is sufficiently short so that the mixing of the two streams is incomplete, and that both streams have isentropic cores. The momentum thickness of the mixing region is obtained from the momentum-integral equation for the turbulent mixing region assuming that momentum and temperature diffuse at the same rate. The momentum thickness at the nozzle exit is related to the initial momentum thickness created by the wall separating the two streams. The exit-momentum thicknesses of the mixing region and the wall are used to obtain the actual thrust coefficient. Experimental data on primary-secondary flow properties and thrust coefficients of a divergent-shroud ejector nozzle show good correlation with the theory.


1969 ◽  
Vol 36 (4) ◽  
pp. 657-663
Author(s):  
J. P. Lamb ◽  
T. F. Greenwood ◽  
J. L. Gaddis

The longitudinal motion equation for turbulent boundary layers is linearized in a manner which retains the spirit of Reichardt’s inductive theory. The resulting approximate velocity profiles for isobaric free shear layers are found to be functions of the density field as well as the velocity of the secondary stream. Using the amount of transverse shift, which is required to satisfy the momentum integral equation, as a figure of merit, it is shown that the alternate profiles are generally better representations of the flow field than distributions obtained with the classic Oseen linearization for both developing and fully developed free layers. The alternate velocity distributions, in combination with integral conservation equations, are shown to yield characteristic velocities in the midpart of the profile which are in agreement with those obtained from more elaborate nonlinear analyses.


1964 ◽  
Vol 86 (4) ◽  
pp. 765-771 ◽  
Author(s):  
R. Curtet ◽  
F. P. Ricou

If it is assumed that the mean-velocity profiles of a ducted jet are similar in form sufficiently for downstream of the orifice it is possible, as shown in earlier papers [1, 2, 3], to integrate the equations of motion using the boundary-layer approximation and assuming a constant-energy secondary stream. It is necessary to know when and how this limiting profile is reached, and whether a similar tendency to self-preservation of the components of the velocity fluctuations is observed before the jet reaches the duct-wall boundary layer. Measurements have been made in an axisymmetric ducted air jet of the mean and fluctuating velocities, jet width, secondary-stream velocity, ductwall static pressure, and the boundary layer thickness. Results are compared with values predicted by the approximate jet theory. The authors define form factors calculated from measured profiles of mean velocities, of radial and longitudinal components of the velocity fluctuations, and of the shear stress. The variation of these form factors indicates a definite tendency to similarity for the mean velocity profiles; however, departures from similarity persist for the velocity fluctuations to the limit of measurements, about three duct diameters (40 nozzle diameters).


2009 ◽  
Vol 8 (3) ◽  
pp. 261-282 ◽  
Author(s):  
Mikel Alonso ◽  
Eldad J. Avital

Sound generation by low speed circular and elliptic coaxial jets is investigated computationally. The secondary to primary jet velocity ratio is limited up to 0.4 and the elliptic jet profile has a 2:1 aspect ratio. Large Eddy Simulations are coupled with the Lighthill's acoustic analogy. Flow incompressibility is assumed limiting the study to the compact quadrupole structures generated during the jet mixing process. As expected, adding a secondary stream is found to extend the mixing region, while changing the jet geometry from circular to elliptic leads to vice versa. Good qualitative agreement in the flow behaviour is achieved with known results. Lighthill's longitudinal streamwise quadrupole is found to dominate the sound generation leading to a mildly high streamwise emission. Increasing the velocity ratio of the secondary stream to the primary stream increases the dominance of the streamwise sound emission. Good qualitative agreement with a previously suggested sound directivity pattern is achieved. Adding a secondary stream to the jet is found to have a mixed effect on the emitted acoustic power. A plausible explanation based on a large scale instability wave model is presented. Dominance of the longitudinal streamwise quadrupole Qxx was observed in all jets and the lateral quadrupoles Qxy and Qxz were of about the same magnitude and only secondary to Qxx. This resulted in high sound emission in the streamwise direction particularly as U1 /U0 was increased to 0.4. Good qualitative agreement was found with a previously suggested expression for the sound directivity pattern [18]. Adding a secondary stream did not cause a significant reduction in the overall acoustic power output as changing the jet geometry from circular to elliptic which was also limited to about 2 dB reduction. Further evidence for the existence of a large scale wave packet structure in the mixing region was produced. The wave packet source model was used to point to the opposing effects on the acoustic power output when adding a secondary stream, which could result in its mild and mixed effect.


2015 ◽  
Vol 75 (2 suppl) ◽  
pp. 91-97 ◽  
Author(s):  
D Endres Júnior ◽  
MH Sasamori ◽  
MBB Cassanego ◽  
A Droste

<p>The <italic>Tradescantia</italic> micronucleus (Trad-MCN) bioassay was used to investigate genotoxicity of water bodies in the Parque Municipal Henrique Luís Roessler (PMHLR), a conservation unit in the city of Novo Hamburgo, Southern Brazil, from November 2010 to October 2011. Every month, cuttings with young inflorescences of <italic>Tradescantia pallida</italic> var. <italic>purpurea</italic> were exposed for 24 hours to water collected at three sites in the park: (S1) head of the main stream; (S2) head of a secondary stream; (S3) a point past the junction of the two water bodies in which S1 and S2 were located. As a negative control, cuttings were exposed to distilled water for 24 h every quarter. Micronuclei (MCN) frequency was determined in young tetrads of pollen mother cells and described as MCN/100 tetrads. Rainfall data were also recorded. In nine months at S1 and S2, and in eleven months at S3, micronuclei frequencies were significantly higher than in quarterly controls, in which frequencies varied from 1.19 to 1.62.</p><p>During sampling, no significant differences were found in MCN frequencies at S1, which ranged from 2.2 to 3.6. At the other sampling sites, there were significant differences between the months evaluated, and MCN frequencies ranged from 1.3 to 6.5 at S2 and from 2.3 to 5.2 at S3. There were no associations between rainfall and MCN frequencies at the three sampling sites. <italic>Tradescantia pallida</italic> var. <italic>purpurea</italic>confirmed genotoxicity in the water bodies of the PMHLR, even at the head of the streams, which suggests that actions should be promoted to control anthropogenic effects in the streams of this conservation unit.</p>


Author(s):  
Meng Liu ◽  
Na Zhang

The authors proposed an ammonia-water cycle for power and refrigeration cogeneration which employs a splitting and absorption unit to adjust the desired solution concentrations. Energy efficiency and exergy efficiency of this cycle are found to be 27.3% and 57.6%, respectively, at the cycle highest heat addition conditions of 450°C /111bar. Nevertheless, a large exergy destruction takes place in the heat transfer and throttling process of this cycle. In this paper, three proposals are investigated to recover the energy of the heat transfer and throttling process. The weak ammonia/water solution is superheated by internal heat recovery, and then its energy is converted into useful outputs by: 1) sending the superheated ammonia-weak stream into the turbine, and the energy is directly converted into the power output: 2) and 3) introducing an ejector to the cycle, the superheated stream is used as the primary stream, the turbine exhaust and the evaporator outlet stream are used as the secondary stream, respectively, the energy is indirectly convert into power or refrigeration output. Simulations show that the three proposals enable the increments of 2.9%, 0.8% and 0.7%, respectively, in the exergy efficiency over the base cycle. Obviously, the first proposal has superiority in term of the thermal performance, while the latter two proposals have some advantages in respect of the operation, maintenance and capital costs.


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