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1.
雷暴低空风切变中大雨对飞行的影响 总被引：8，自引：0，他引：8
王永忠 《南京气象学院学报》2006,29(1):136-140
分析了雷暴低空风切变中大雨滴冲击飞机的机身和机翼而引起的水平和垂直动量损失，估算了大雨累计在机身和机翼上的水膜厚度，并讨论了因遇到大雨雨滴冲撞而粗糙化的机体所产生的阻力。结果表明：雷暴低空风切变中大雨雨滴的冲击作用是明显的，被粗糙化的机体所产生的阻力能显著改变飞行轨迹，并能影响飞行安全；累计在机身和机翼上的水膜厚度造成的飞机质量的增加对飞行的影响可以忽略。 相似文献
2.
地形影响的飞机颠簸及其数值仿真实验 总被引：1，自引：1，他引：1
首先利用中尺度数值模式ARPS模拟气流过山生成飞行数值仿真所需要的风场，然后利用飞机载荷因数变量方程进行飞机飞行的数值仿真试验。研究结果表明，气流过山产生的山脉重力波由于风切变临界层破碎，一方面能在对流层产生较强的湍流引起晴空飞机颠簸，另一方面也能在山脉背风面产生强烈下坡风，背风转子环流及低空湍流，影响飞机的起飞和着陆。揭示了飞机在过山脉地形背风面所产生的大气湍流中飞行时引起飞机颠簸的物理机制，有助于增强飞机颠簸的预测能力和飞行气象保障能力。 相似文献
3.
Dr. D. P. Jorgensen T. Matejka J. D. DuGranrut 《Meteorology and Atmospheric Physics》1996,59(1-2):83-104
Summary Two techniques for deriving horizontal and vertical air motions using vertically scanning airborne Doppler radar data are presented and discussed. These techniques make use of the scanning ability of the NOAA P-3 tail-mounted radar antenna to view a region of space from at least two vantage points during a straight-line flight track. The scanning methodology is termed the Fore/Aft Scanning Technique or FAST because the antenna is alternately scanning forward and then aft of the flight track. The major advantages of FAST over flying two quasi-orthogonal flight tracks with the antenna scanning normal to the flight track are that the data are collected in roughly half the time and the aircraft does not have to execute a right-angle turn. However, accuracy of the resulting wind field is compromised slightly because the beam intersection angle is reduced from 90° to about 50°. The reduction of area covered because of large drift angles is also discussed.A three-dimensional wind field can be constructed using the dual-Doppler equations from FAST data using the two radial velocity estimates and vertical integration of the continuity equation with a boundary condition of no vertical motion at cloud top and the Earth's surface. To keep errors in the calculated winds acceptably small, the elevation angles are typically restricted to ±45° from the horizontal to minimize contamination of the horizontal wind by terminal fallspeeds.A different, and perhaps more believable vertical velocity, can be derived using a second technique that utilizes two (or more) airborne Doppler radar equipped aircraft each using FAST to observe the echo-top vertical velocity at common point (e.g., two aircraft flying parallel flight, paths, or by using an L-shaped flight track with a single aircraft). This technique results in 4 (or more) radial velocity estimates at each point (hence is called the quad-Doppler technique). Horizontal winds can be derived using either an overdetermined three-equation solution or an overdetermined dual-Doppler solution, whichever is more accurate. For the calculation of vertical velocity a new approach is proposed that utilizes the overdetermined triple-Doppler solution for vertical particle motion near cloud top, minus an estimate of terminal fallspeeds, as a top boundary condition for the downward vertical divergence integration to derive vertical air velocity elsewhere in the domain. In addition, this approach allows measurements at steep elevation angles allowing for more depth of coverage for a given range.To show the utility of the method, analyses of data collected using FAST are compared to conventional dual-Doppler-derived wind fields constructed from data collected simultaneously by S-band ground-based Doppler radars. An example of the quad-Doppler technique is also presented from the recently completed Tropical Oceans/Global Atmospheres Coupled Ocean/Atmosphere Response Experiment (TOGA/COARE). Comparisons of quad-Doppler vertical velocity are made with in-situ derived vertical air motions collected by the NASA DC-8 to judge the quality of the approach.With 9 Figures 相似文献
4.
Karl E. Garman Phil Wyss Mark Carlsen James R. Zimmerman Brian H. Stirm Thomas Q. Carney Robert Santini Paul B. Shepson 《Boundary-Layer Meteorology》2008,126(3):461-476
Aircraft-based vertical flux measurements fill a gap in the spatial domain for studies of biosphere–atmosphere exchange. To
acquire valid flux data, a determination of the deviation from the mean vertical wind, w′, is essential. When using aircraft platforms, flux measurements are subject to systematic and random errors from airflow
distortion caused by the lift-induced upwash ahead of the aircraft. Although upwash is typically considered to be a constant
quantity over periods used for calculating fluxes, it can vary significantly over short (and longer) periods due to changes
in aircraft lift. The characterization of such variations in upwash are of undeniable importance to flux measurements, especially
when real-time computations of w′ are required. In this paper, the variability in upwash was compared to the calculated upwash from the model of Crawford
et al. (Boundary-Layer Meteorol, 80:79–94, 1996) using data taken during a long-period (phugoid mode) free oscillation of
the aircraft. The cyclic variation of lift during the free oscillation offers an ideal scenario in which to acquire in-flight
data on the upwash that is present, as well as to test the capability of upwash correction models. Our results indicate that
while this model corrects for much of the mean upwash, there can be significant variations in upwash on a time scale that
is important to flux measurements. Our results suggest that use of the measured load factor could be an easily implemented
operational constraint to minimize uncertainty in w′ due to changing upwash from changing aircraft lift. We estimate, using the phugoid data, and from variations in aircraft
attitude and airspeed in flux-measurement configuration, that the uncertainty in w caused by variable upwash is approximately ± 0.05 m s−1. 相似文献
5.
How Well Can We Measure the Vertical Wind Speed? Implications for Fluxes of Energy and Mass 总被引：2，自引：2，他引：0
John Kochendorfer Tilden P. Meyers John Frank William J. Massman Mark W. Heuer 《Boundary-Layer Meteorology》2012,145(2):383-398
Sonic anemometers are capable of measuring the wind speed in all three dimensions at high frequencies (10–50 Hz), and are relied upon to estimate eddy-covariance-based fluxes of mass and energy over a wide variety of surfaces and ecosystems. In this study, wind-velocity measurement errors from a three-dimensional sonic anemometer with a non-orthogonal transducer orientation were estimated for over 100 combinations of angle-of-attack and wind direction using a novel technique to measure the true angle-of-attack and wind speed within the turbulent atmospheric surface layer. Corrections to the vertical wind speed varied from −5 to 37% for all angles-of-attack and wind directions examined. When applied to eddy-covariance data from three NOAA flux sites, the wind-velocity corrections increased the magnitude of CO2 fluxes, sensible heat fluxes, and latent heat fluxes by ≈11%, with the actual magnitude of flux corrections dependent upon sonic anemometer, surface type, and scalar. A sonic anemometer that uses vertically aligned transducers to measure the vertical wind speed was also tested at four angles-of-attack, and corrections to the vertical wind speed measured using this anemometer were within ±1% of zero. Sensible heat fluxes over a forest canopy measured using this anemometer were 15% greater than sensible heat fluxes measured using a sonic anemometer with a non-orthogonal transducer orientation. These results indicate that sensors with a non-orthogonal transducer orientation, which includes the majority of the research-grade three-dimensional sonic anemometers currently in use, should be redesigned to minimize sine errors by measuring the vertical wind speed using one pair of vertically aligned transducers. 相似文献
6.
气象条件对体育比赛有着重要的作用,温度、湿度、降水、风等各种气象因素对体育比赛项目都会产生一定的影响。使用自20世纪80年代以来国内外有关气象条件对标枪项目的影响、标枪训练与投掷的技术标准、标枪项目的生物力学等方面的文献资料和有关标枪风洞实验的有关数据,重点分析了风力和风向对标枪投掷的影响。结果表明:在风速较小(顺风和侧风时风速小于6 m/s,在逆风时风速小于3 m/s)的情况下,一定的风速使标枪的飞行距离稍有增加,当风速超过6 m/s以后,飞行距离随风速的加大而减少。另外,气温和湿度对标枪运动的影响主要是在对运动员的身体状态方面,表现为对运动员的心理和生理的影响,影响运动员水平的发挥,降水、大雾等则表现为能见度差,造成比赛中止甚至取消。 相似文献
7.
单部多卜勒天气雷达探测低空风切变方法 总被引：5，自引：0，他引：5
利用单多卜勒天气雷达风场资料对一维径向、一维方位、二维复合风切变值进行了计算 ,并对机场附近飞机所受气流速度变化进行分析。所得结果旨在定量描述机场附近低空风切变区 ,检验对下击暴流、中气旋、阵风锋探测的结果 ,确定飞机起降潜在危险区。 相似文献
8.
Timothy L. Crawford Robert T. McMillen Ronald J. Dobosy Ian MacPherson 《Boundary-Layer Meteorology》1993,66(3):237-245
Airplane aerodynamic characteristics correlate aircraft speed with vertical wind velocity, making the time average inappropriate for estimating the ensemble average in airborne eddy-correlation flux computations. The space average, the proper form, is implemented as a time integral by a transformation of variables, which can be interpreted as a ground-speed correction to the time average. The mathematical forms are presented, and the importance of the speed correction is illustrated with airborne data. The computed correction is found to be highly variable, depending on both the turbulent flow encountered and the aircraft used. In general, the speed connection becomes more important as airplane size is reduced. For a small, single-engine Long-EZ airplane, used as an example, the straight time average erred, half the time, by 12%, 10%, 20%, and 15%, respectively, for computed fluxes of momentum, heat, moisture, and CO2. For a much heavier Twin Otter airplane, also used as an example, the straight time average erred, half the time by only 1%. These errors increased with decreasing altitude for the Long-EZ and with increasing altitude for the Twin Otter.Oak Ridge Associated Universities, assigned to NOAA/ATDD. 相似文献
9.
The Campbell CSAT3 sonic anemometer is one of the most popular instruments for turbulence measurements in basic micrometeorological research and ecological applications. While measurement uncertainty has been characterized by field experiments and wind-tunnel studies in the past, there are conflicting estimates, which motivated us to conduct a numerical experiment using large-eddy simulation to evaluate the probe-induced flow distortion of the CSAT3 anemometer under controlled conditions, and with exact knowledge of the undisturbed flow. As opposed to wind-tunnel studies, we imposed oscillations in both the vertical and horizontal velocity components at the distinct frequencies and amplitudes found in typical turbulence spectra in the surface layer. The resulting flow-distortion errors for the standard deviations of the vertical velocity component range from 3 to 7%, and from 1 to 3% for the horizontal velocity component, depending on the azimuth angle. The magnitude of these errors is almost independent of the frequency of wind speed fluctuations, provided the amplitude is typical for surface-layer turbulence. A comparison of the corrections for transducer shadowing proposed by both Kaimal et al. (Proc Dyn Flow Conf, 551–565, 1978) and Horst et al. (Boundary-Layer Meteorol 155:371–395, 2015) show that both methods compensate for a larger part of the observed error, but do not sufficiently account for the azimuth dependency. Further numerical simulations could be conducted in the future to characterize the flow distortion induced by other existing types of sonic anemometers for the purposes of optimizing their geometry. 相似文献
10.
本文研究了斜压效应对地转动量Ekman流的影响。利用两变量奇异摄动方法求得了边界层中风场及顶部垂直速度的前二级一致有效渐近解析解,解中明显地反映了斜压情形地转风随高度变化(即热成风)的影响,尤其是其中一级近似解完全由热成风影响所致。在边界层顶垂直速度的解中导出了三种由斜压效应引起的Ekmon抽吸新物理因子,即热成风形变、热成风涡度及热成风涡度交叉项等抽吸因子。分析表明,这些因子只在具有水平温度梯度不均匀的系统(譬如锋区)中方能出现。文中还对锋区内上述三种抽吸因子的动力特征作了具体的分析,指出在锋区这样的强斜压系统中,此三种抽吸因子的贡献是显著的。下一文中,我们将利用本文所得理论解对斜压效应进行具体的定量计算。 相似文献
11.
Mean flow, turbulence, and surface pressure measurements over an escarpment are presented. The speed-up in the mean wind field shows the known dependence on stratification. Cross-sections of the standard deviation of horizontal and vertical wind components and of the friction velocity are derived from the data and compare favorably with the numerical model of Zeman and Jensen (1987). The modification of turbulent power spectra at intermediate frequencies can be explained by rapid distortion theory. At very low frequencies, there is a quasi-stationary response to the disturbance. Except for speed-up and standard deviations of the wind components, which are also shown for downslope wind, all results in this paper refer to upslope winds.An analysis of the vertical momentum flux reveals that upstream of the escarpment, most of the flux is transported in sweeps of fast, sinking motion to the ground. Downstream of the escarpment, ejections of slow, rising motion dominate the turbulent transport. 相似文献
12.
M. G. Mennen H. J. M. A. Zwart J. E. M. Hogenkamp J. W. Erisman 《Boundary-Layer Meteorology》1996,81(3-4):353-371
Flow distortion errors on wind and friction velocity induced by a box simulating the housing of a gas analyzer used in dry
deposition eddy correlation measurements were determined in a field experiment. ‘Undisturbed’ and ‘disturbed’ wind and friction
velocities, measured with two dry deposition monitoring systems run simultaneously, were compared, one to the other. In the
‘disturbed’ case the box was mounted below the 3-component probe of the sonic anemometer of one of these systems, while in
the ‘undisturbed’ case the box was removed. When the probe was located on the upstream side of the box, the results showed
satisfactory agreement with theoretical estimates using Wyngaard’s potential-flow approach and a spherical model for the box.
This model can be applied to obtain first-order corrections for flow distortion errors induced by cubic-like (or spherical)
obstacles such as a gas analyzer housing used in dry deposition research systems, or to determine the optimal location of
this housing relative to the sonic probe in such systems. When the probe was located halfway downstream and halfway to the
side of the box, the experimental flow distortion errors did not exceed those for the upstream case. This implies that to
keep flow distortion errors in dry deposition systems as small as possible the sonic probe can be placed upstream but also
to the side of the gas analyzer housing. The results of our experiments also confirmed that correcting for flow distortion
with the commonly used tilt equations yields underestimated values. 相似文献
13.
The theory, configuration, and accuracy of an inexpensive probe to measure turbulence from a small airplane are presented. The probe employs a nine-hole pressure-sphere design along with inprobe high-frequency pressure, temperature, and acceleration sensors. This sensor suite is specifically designed to extend mass, momentum and energy eddy-flux measurement to the higher frequencies characteristic of marine and nocturnal boundary layers. The probe is part of a mobile flux system, independent of the conveyance, which does not require a separate Inertial Navigation System.The new nine-port pressure sphere turbulence probe allows accurate turbulent velocity measurement with proper probe installation and appropriate computation technique for dynamic pressure. A thermistor in the central pressure port provides simultaneous temperature measurement, at a location symmetrical with respect to the flow, for accurate determination of true airspeed and heat flux. The probemounted temperature sensor gives heat fluxes with variance 5% of the mean in a weakly-turbulent marine boundary layer.Oak Ridge Associated Universities, assigned to NOAA/ATDD. 相似文献
14.
Gary K. Greenhut 《Boundary-Layer Meteorology》1981,20(1):75-100
The momentum flux data obtained by the gust probe aboard the NOAA DC-6 aircraft during GATE are analyzed. Vertical profiles are obtained for Phases I and III and correlated with vertical wind velocity profiles using the geostrophic departure method. Reasonable agreement is obtained using the horizontal equations of motion with negligible advective acceleration. The vertical profiles of momentum flux and wind speed variance compare well with the numerical model results of Deardorff (1972) and Wyngaard et al. (1974). Vertical distributions of power spectra for vertical eddy motion and cospectra corresponding to the momentum flux components are obtained along with the height variation of the dominant length scales of vertical eddy motion and the dissipation rate of turbulence kinetic energy. When normalized by mixed-layer similarity, these results agree well with previous determinations in the boundary layer over tropical oceans and over land. 相似文献
15.
L&#; Naiping Li Shiming Chen Yanjuan Chen Jingnan Zheng Yueming 《Acta Meteorologica Sinica》1987,1(1):96-104
In this paper,a comparison is made of the Doppler sodar wind measurement with the in-situ measurements on a 325 m meteorological tower.The results show that when the ratio of signal to noise is larger than 1,the mean wind speeds and directions obtained from the two techniques are well correlated,thus their profiles are close to each other.The mean value and root mean square of vertical velocity measured by the Doppler sodar are a little larger than those measured by a sonic anemometer at a height of 85 m,which is in agreement with the analysis by Gaynor et al.(1983).We notice that there are some differences in the observational results between the Doppler sodar and insitu measurements,especially when comparing the values measured at each time.Therefore,it is important to analyze the reason for the differences and to make corrections to the Doppler sodar measurements. 相似文献
16.
北京325 m气象塔塔体对测风影响的数值模拟 总被引：1，自引：0，他引：1
安装在气象观测塔上的仪器进行风速测量时,气象塔塔体本身会对流场有一定的影响,使其附近局部流场发生变化,产生绕流和尾流,导致所测风场数据相对于真实风场值失真,利用计算流体力学软件Fluent对北京325m框架式气象塔周围的风场进行了模拟,给出流向风速在该塔伸臂上测风位置的失真情况,及风速失真大小随风向风速的变化规律,计算表明若伸臂处于迎风面,在测风点上的风速误差均小于5%,与实际观测一致,验证了北京325m气象塔风速伸臂设计的合理性。 相似文献
17.
In this paper,a scheme of dual-Doppler radar wind analysis based on a three-dimensional variational method is proposed and performed in two steps.First,the horizontal wind field is simultaneously recovered through minimizing a cost function defined as a radial observation term with the standard conjugate gradient method,avoiding a weighting parameter specification step.Compared with conventional dual-Doppler wind synthesis approaches,this variational method minimizes errors caused by interpolation from radar observation to analysis grid in the iterative solution process,which is one of the main sources of errors.Then,through the accelerated Liebmann method,the vertical velocity is further reestimated as an extra step by solving the Poisson equation with impermeable conditions imposed at the ground and near the tropopause.The Poisson equation defined by the second derivative of the vertical velocity is derived from the mass continuity equation.Compared with the method proposed by O’Brien,this method is less sensitive to the uncertainty of the boundary conditions and has better stability and reliability.Furthermore,the method proposed in this paper is applied to Doppler radar observation of a squall line process.It is shown that the retrieved vertical wind profile agrees well with the vertical profile obtained with the velocity–azimuth display(VAD)method,and the retrieved radial velocity as well as the analyzed positive and negative velocity centers and horizontal wind shear of the squall line are in accord with radar observations.There is a good correspondence between the divergence field of the derived wind field and the vertical velocity.And,the horizontal and vertical circulations within and around the squall line,as well as strong updrafts,the associated downdrafts,and associated rear inflow of the bow echo,are analyzed well.It is worth mentioning that the variational method in this paper can be applied to simultaneously synthesize the three-dimensional wind field from multiple-Doppler radar observations. 相似文献
18.
19.
下投式飞机和火箭焰弹分散的催化剂一般都形成若干条垂直线源。该文利用湍流扩散的梯度输送理论,提出了层状云中垂直线源催化剂扩散的理论模式,并给出了顺风向和垂直于风向发射的多条线源催化剂浓度叠加效应的计算公式。 相似文献
20.
Patricia Jones Boyle Kenneth L. Davidson Donald E. Spiel 《Dynamics of Atmospheres and Oceans》1987,10(4)
Surface stress values obtained from the NOAA Ship OCEANOGRAPHER during STREX indicate that wind speed and stability dependent bulk derived stress values are two to three times too low in surface pre-frontal, pre-trough and pre-ridge regions of transiting synoptic systems. The measured stress values were based on calculations of turbulent kinetic energy dissipation rates using hot film measured velocity variances. Bulk stress values obtained with wind speed (neutral drag coefficient) and stability dependencies in the Large and Pond derivation agreed very well with the measured values in other regions of the synoptic systems. In situ wave information was not adequate to relate differences to coupled vector wind and wave fields. However, analyses and interpretation of wind and stability effects suggest that wind wave interaction was the reason for the observed sub-synoptic (mesoscale) stress enhancements. 相似文献