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1 , but such winds are required to be slightly supersonic.
2                                     By using supersonic air flow, the nebulator produces drops that a
3    A numerical approach is used to model the supersonic air stream and cross-jet flow with the SST tu
4 atitude origin, implying that emissions from supersonic aircraft could reach the middle stratosphere.
5 rature such a phenomenon is documented for a supersonic airfoil leading edge injection.
6 can), 2-dimensional shear wave elastography (Supersonic Aixplorer), and liver biopsy after an overnig
7 which is fundamental to our understanding of supersonic and hypersonic compressible turbulence.
8                Shock waves, the interface of supersonic and subsonic plasma flows, are the primary re
9 surface of rod electrode via high efficiency supersonic atmospheric plasma spraying method.
10     Benzene clusters are generated by pulsed supersonic beam expansion, ionized by electron impact, m
11                   This beam was crossed by a supersonic beam of D2.
12                              In a coexpanded supersonic beam, we have studied the rotationally inelas
13 ture by using a buckminsterfullerene (C(60)) supersonic beam.
14 New PES data are obtained using Ar-seeded He supersonic beams to achieve better cluster cooling, resu
15  cryogenic buffer-gas cooling or decelerated supersonic beams).
16 horse in motion and the 1887 photograph of a supersonic bullet.
17 rom the curved compressed shear layer of the supersonic but surprisingly laminar jet.
18                            Specifically, the supersonic Cerenkov wave pattern was observed at room te
19 n cluster (C13) has been observed by using a supersonic cluster beam-diode laser spectrometer.
20                                              Supersonic cold spraying is an emerging technique for ra
21               Alternatively, detonation is a supersonic combustion-driven shock offering several adva
22 be nozzle for the injection of fuel jet in a supersonic combustor of a scramjet engine in the existen
23                            The properties of supersonic, compressible plasma turbulence determine the
24 /-0.6 microm were accelerated by a hand-held supersonic device to impact freshly excised porcine skin
25 n nucleation occurs near the shock front and supersonic dislocation motion lasts just fractions of pi
26 alysis, but many of the peculiarities of the supersonic dislocations are dominated by nonlinear effec
27 an the speed of sound if they are created as supersonic dislocations at a strong stress concentration
28          Since the theoretical prediction of supersonic dislocations over half a century ago, there i
29 f an electron-phonon Cerenkov instability at supersonic drift velocities.
30 ))(m)(-) clusters carried out in an ionized, supersonic entrainment ion source.
31 ng a reaction tube designed to constrain the supersonic expansion and increase the collision cooling
32  and trapping conformational population in a supersonic expansion are discussed.
33 ra of molecular clusters generated in a cold supersonic expansion by means of highly resolved spectro
34 aporization of a graphite target followed by supersonic expansion of the vaporized material within a
35 mics reveals that the low temperature of the supersonic expansion plays a key role in forming these c
36 d out in the cold, isolated environment of a supersonic expansion to explore its intrinsic UV spectra
37 roadband rotational spectroscopy in a pulsed supersonic expansion unambiguously identifies all three
38 ration of a hydrocarbon precursor undergoing supersonic expansion.
39  (ZG5-NHMe) in the isolated environment of a supersonic expansion.
40 ulsed valve to cool and isolate CH(2)OO in a supersonic expansion.
41 ed out on the isolated molecules cooled in a supersonic expansion.
42 -NHMe (alphabetaL), isolated and cooled in a supersonic expansion.
43 cals with HONO(2) and stabilized in a pulsed supersonic expansion.
44 porization of a graphite rod and cooled in a supersonic expansion.
45 nd considering collisional relaxation in the supersonic expansion.
46 nal spectra of the water hexamer recorded in supersonic expansions.
47 liable propulsion systems for hypersonic and supersonic flight.
48 yager 1 crossed the termination shock of the supersonic flow of the solar wind on 16 December 2004 at
49 This model is suitable for both subsonic and supersonic flows with or without chemical reaction and/o
50 g edge shock topology and flow structures in supersonic flows.
51 ids to scatterless polariton superfluids and supersonic fluids-all at room temperature, clear consequ
52 shaped gas nozzles providing centimeter-long supersonic gas jets that can be used as targets for the
53                                              Supersonic gas motions left over from the Big Bang preve
54            By contrast, observations of cold supersonic H(+) flowing out of the polar ionosphere(8,9)
55                              Shock waves are supersonic high-amplitude pressure waves that cause baro
56                                Using uniform supersonic hydrogen flows we can now report direct exper
57                       However, in explosive, supersonic, hypersonic, cavitating, or ionizing environm
58 two-dimensional shear-wave elastography with SuperSonic Imagine [2D-SWE-SSI]) and the added value of
59 using the ultrasound (US) system, Aixplorer (SuperSonic Imagine S.A., Aix-en-Provence, France), TE us
60 antly higher when an SC6-1 probe (Aixplorer; SuperSonic Imagine SA, Aix-enProvence, France) was used
61                Twenty observational studies (SuperSonic Imagine, General Electric Healthcare, and Can
62                                       Steady supersonic injection yields the largest abatement in the
63 s through the local interstellar medium, its supersonic, ionized solar wind carves out a cavity calle
64 lysis in the presence of the gas driving the supersonic jet (He, Ne, and N(2)) in the GC-MRR.
65 d from formic acid and sulfur trioxide under supersonic jet conditions.
66 ectrometry coupled with laser desorption and supersonic jet cooling is described.
67                                          The supersonic jet cools the analytes to ~2 K, resulting in
68 er cluster ion beam has been developed using supersonic jet expansion methodologies that enable ion y
69 clic alkaloid (5S, 6S, 7R, 11R)-matrine in a supersonic jet expansion, using chirped-pulsed broadband
70              With a Fabry-Perot cavity and a supersonic jet incorporated into a GC-MRR, dramatic impr
71 citation and dispersed emission methods in a supersonic jet to investigate the electronic states invo
72 citation and dispersed emission methods in a supersonic jet to investigate the nature of the electron
73  detection of five different structures in a supersonic jet.
74 een observed by rotational spectroscopy in a supersonic jet.
75         Other techniques, such as the use of supersonic jets and cryogenic buffer gases, have reached
76 : molecules in condensed phases, isolated in supersonic jets and helium nanodroplets, and, recently a
77  also by its expulsion in the form of highly supersonic jets that can stretch for several parsecs(1,2
78 mensional micro-architected materials, where supersonic microparticles to velocities of up to 850 m/s
79 lusters are produced in a laser-vaporization supersonic molecular beam and characterized by photoelec
80  report the detection of gas-phase HOON in a supersonic molecular beam by Fourier transform microwave
81  carbenes, H2C5 and H2C6, were detected in a supersonic molecular beam by Fourier transform microwave
82 equilibrium on rutile-TiO2(110) by combining supersonic molecular beam, scanning tunneling microscopy
83 ourier transform microwave spectroscopy of a supersonic molecular beam, the rotational spectrum of th
84 a pulsed discharge ion source coupled with a supersonic molecular beam.
85  employs a traditional micro ESI source with supersonic nebulizing gas.
86 lecular dynamics simulations which show that supersonic partial dislocation bursts play a role in tri
87 tions of shocked silicon to reveal transient supersonic partial dislocation motion at approximately 1
88                                 We show that supersonic radial propagation of CMEs away from the Sun
89 g high-power laser facilities to investigate supersonic radiation-dominated waves.
90 s, or detonations, which are ultrahigh-speed supersonic reaction waves.
91 eir frequency range as the qubit reaches the supersonic regime, similar to Cherenkov radiation.
92 ver stiffness measurement (LSM) evaluated by supersonic shear imaging (SSI), FibroScan, and acoustic
93               When subjected to 1.5 km s(-1) supersonic shots, TSAMs were shown to absorb the impact
94 oximately 34 degrees N), then re-entered the supersonic solar wind about 200 days later at approximat
95 cs dominated interaction regions between the supersonic solar wind and a Solar System object.
96      We argue that the spacecraft exited the supersonic solar wind and passed into the subsonic regio
97 n shock that marks the abrupt slowing of the supersonic solar wind and the beginning of the extended
98                     A transition between the supersonic solar wind and the subsonic heliosheath was o
99 ellar medium, continuously emitting ionized, supersonic solar wind plasma and carving out a cavity in
100                          The prediction of a supersonic solar wind(1) was first confirmed by spacecra
101 to heat the corona but also to originate the supersonic solar wind.
102 on of TA phonons when the electrons approach supersonic speed, and (iii) the onset of elastic inter-L
103  operating engines, the fuel jets can exceed supersonic speeds and result in gaseous shock waves.
104               The films are deposited by the supersonic spraying technique, which facilitates the rap
105 ithout the need for ultraviolet backgrounds, supersonic streaming motions or even atomic cooling.
106 om the Sun where the solar wind changes from supersonic to subsonic flow.
107 ed of bath-excitation propagation, e.g., for supersonic transfer through phonon baths.
108 ly the statistical behavior of boundary-free supersonic turbulence created by the collision of two la
109                    Cold flows drive violent, supersonic turbulence in the halo, which prevents star f
110                                              Supersonic turbulence occurs in many environments, parti
111 pplied to conduct dimensionless learning for supersonic turbulence, aerodynamic drag on both smooth a
112 ting apparatus to selectively launch them at supersonic velocities (~400 meters per second).
113 microparticles impact metallic substrates at supersonic velocities.
114 ume is liquid water, with gas accelerated to supersonic velocity in nozzle-like channels.
115   Simulation results show that the localized supersonic water hammer created by an asymmetrical bubbl
116 unexpected finding is that the flow is still supersonic with respect to the thermal ions downstream o
117 curs where the solar wind changes from being supersonic (with respect to the surrounding interstellar
118 alistic internal mass distribution or highly supersonic zonal winds.

 
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