Low Level Wind Shear
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Low Level Wind Shear: Invisible Enemy to Pilots
Low Level Wind Shear: Invisible Enemy To Pilots On the afternoon of August 2, 1985, a landmark aircraft accident occurred at the Dallas/Fort Worth (DFW) airport. The tragic accident, which killed 137 of the 163 passengers on board Delta Airlines Flight 191, was responsible for making “wind shear” a more commonly known weather phenomenon and implementing many new changes with regard to wind shear detection (Ref. 1). On that day, thunderstorms were in the area of approach to runway 17L at the DFW International Airport, with a thunderstorm rain shaft right in the path of final approach. The crew decided to proceed through the thunderstorm, which turned out to be a critical error. Shortly after entering the storm, turbulence increased and the L1011 aircraft encountered a 26 knot headwind. Just as suddenly, the wind switched to a 46 knot tailwind, resulting in a loss of 72 knots of airspeed. This much of an airspeed loss on final approach, when the jet was only 800 feet above the surface, was unrecoverable and the aircraft eventually crashed short of the runway (Ref. 1). The sudden change in wind speed and direction that the aircraft encountered is called wind shear. Wind shear can occur at many different levels of the atmosphere, however it is most dangerous at the low levels, as a sudden loss of airspeed and altitude can occur. Plenty of altitude is normally needed to recover from the stall produced by the abrupt change in wind speed and direction, which is why pilots need to be aware of the hazards and mitigation of low-level wind shear. -
3. Electrical Structure of Thunderstorm Clouds
3. Electrical Structure of Thunderstorm Clouds 1 Cloud Charge Structure and Mechanisms of Cloud Electrification An isolated thundercloud in the central New Mexico, with rudimentary indication of how electric charge is thought to be distributed and around the thundercloud, as inferred from the remote and in situ observations. Adapted from Krehbiel (1986). 2 2 Cloud Charge Structure and Mechanisms of Cloud Electrification A vertical tripole representing the idealized gross charge structure of a thundercloud. The negative screening layer charges at the cloud top and the positive corona space charge produced at ground are ignored here. 3 3 Cloud Charge Structure and Mechanisms of Cloud Electrification E = 2 E (−)cos( 90o−α) Q H = 2 2 3/2 2πεo()H + r sinα = k Q = const R2 ( ) Method of images for finding the electric field due to a negative point charge above a perfectly conducting ground at a field point located at the ground surface. 4 4 Cloud Charge Structure and Mechanisms of Cloud Electrification The electric field at ground due to the vertical tripole, labeled “Total”, as a function of the distance from the axis of the tripole. Also shown are the contributions to the total electric field from the three individual charges of the tripole. An upward directed electric field is defined as positive (according to the physics sign convention). 5 5 Cloud Charge Structure and Mechanisms of Cloud Electrification Electric Field Change Due to Negative Cloud-to-Ground Discharge Electric Field Change Due to a Cloud Discharge Electric Field Change, kV/m Change, Electric Field Electric Field Change, kV/m Change, Electric Field Distance, km Distance, km Electric field change at ground, due to the Electric field change at ground, due to the total removal of the negative charge of the total removal of the negative and upper vertical tripole via a cloud-to-ground positive charges of the vertical tripole via a discharge, as a function of distance from cloud discharge, as a function of distance from the axis of the tripole. -
The Difference Between Higher and Lower Flap Setting Configurations May Seem Small, but at Today's Fuel Prices the Savings Can Be Substantial
THE DIFFERENCE BETWEEN HIGHER AND LOWER FLAP SETTING CONFIGURATIONS MAY SEEM SMALL, BUT AT TODAY'S FUEL PRICES THE SAVINGS CAN BE SUBSTANTIAL. 24 AERO QUARTERLY QTR_04 | 08 Fuel Conservation Strategies: Takeoff and Climb By William Roberson, Senior Safety Pilot, Flight Operations; and James A. Johns, Flight Operations Engineer, Flight Operations Engineering This article is the third in a series exploring fuel conservation strategies. Every takeoff is an opportunity to save fuel. If each takeoff and climb is performed efficiently, an airline can realize significant savings over time. But what constitutes an efficient takeoff? How should a climb be executed for maximum fuel savings? The most efficient flights actually begin long before the airplane is cleared for takeoff. This article discusses strategies for fuel savings But times have clearly changed. Jet fuel prices fuel burn from brake release to a pressure altitude during the takeoff and climb phases of flight. have increased over five times from 1990 to 2008. of 10,000 feet (3,048 meters), assuming an accel Subse quent articles in this series will deal with At this time, fuel is about 40 percent of a typical eration altitude of 3,000 feet (914 meters) above the descent, approach, and landing phases of airline’s total operating cost. As a result, airlines ground level (AGL). In all cases, however, the flap flight, as well as auxiliarypowerunit usage are reviewing all phases of flight to determine how setting must be appropriate for the situation to strategies. The first article in this series, “Cost fuel burn savings can be gained in each phase ensure airplane safety. -
Climatic Information of Western Sahel F
Discussion Paper | Discussion Paper | Discussion Paper | Discussion Paper | Clim. Past Discuss., 10, 3877–3900, 2014 www.clim-past-discuss.net/10/3877/2014/ doi:10.5194/cpd-10-3877-2014 CPD © Author(s) 2014. CC Attribution 3.0 License. 10, 3877–3900, 2014 This discussion paper is/has been under review for the journal Climate of the Past (CP). Climatic information Please refer to the corresponding final paper in CP if available. of Western Sahel V. Millán and Climatic information of Western Sahel F. S. Rodrigo (1535–1793 AD) in original documentary sources Title Page Abstract Introduction V. Millán and F. S. Rodrigo Conclusions References Department of Applied Physics, University of Almería, Carretera de San Urbano, s/n, 04120, Almería, Spain Tables Figures Received: 11 September 2014 – Accepted: 12 September 2014 – Published: 26 September J I 2014 Correspondence to: F. S. Rodrigo ([email protected]) J I Published by Copernicus Publications on behalf of the European Geosciences Union. Back Close Full Screen / Esc Printer-friendly Version Interactive Discussion 3877 Discussion Paper | Discussion Paper | Discussion Paper | Discussion Paper | Abstract CPD The Sahel is the semi-arid transition zone between arid Sahara and humid tropical Africa, extending approximately 10–20◦ N from Mauritania in the West to Sudan in the 10, 3877–3900, 2014 East. The African continent, one of the most vulnerable regions to climate change, 5 is subject to frequent droughts and famine. One climate challenge research is to iso- Climatic information late those aspects of climate variability that are natural from those that are related of Western Sahel to human influences. -
Chapter 7.0 – Determining Wind Direction Section 7.1 Overview Of
Chapter 7.0 – Determining Wind Direction Section 7.1 Overview of Wind Direction The wind direction is a measure or indication of where the air movement originated from. The wind direction can be measured through the use of a wind sock, wind vane, or a light object attached to a pole and string (example: A ping pong ball attached to a string which is tied to a stick). Wind direction is generally reported in either Azimuth degrees or Cardinal direction. Azimuth uses a circle with the northern most position indicating 0 degrees. The Cardinal direction system gives an Azimuth degree value a name. For example, 180 degrees is South(S) and 270 degrees is West (W) (See Figure 18 - A basic compass rose). Figure 18 - A basic compass rose Section 7.2 Overview of the homemade Wind Vane The wind vane used in this design was a homemade wind vane using a miniature absolute magnetic shaft encoder. The encoder chosen for use was the MA3 produced by US Digital. The purpose for choosing this specific encoder in regards to this design was that the MA3 met four (4) critical objectives. First, the MA3 was the correct size for the application. Second, the MA3 uses an analog output of 0 volts to 5 volts with respect to the current positions (See Figure 19 – MA3 Output behaviour) Figure 19 – MA3 Output behaviour Third, the MA3 uses a 5 volt input. This was a major consideration when choosing an encoder as a 5 volt input allowed for a more simple integration. Fourth, and final, the MA3 met the requirements of being able to function in an adverse environment, having an operational temperature of -40 ºC to +125 ºC. -
NWS Unified Surface Analysis Manual
Unified Surface Analysis Manual Weather Prediction Center Ocean Prediction Center National Hurricane Center Honolulu Forecast Office November 21, 2013 Table of Contents Chapter 1: Surface Analysis – Its History at the Analysis Centers…………….3 Chapter 2: Datasets available for creation of the Unified Analysis………...…..5 Chapter 3: The Unified Surface Analysis and related features.……….……….19 Chapter 4: Creation/Merging of the Unified Surface Analysis………….……..24 Chapter 5: Bibliography………………………………………………….…….30 Appendix A: Unified Graphics Legend showing Ocean Center symbols.….…33 2 Chapter 1: Surface Analysis – Its History at the Analysis Centers 1. INTRODUCTION Since 1942, surface analyses produced by several different offices within the U.S. Weather Bureau (USWB) and the National Oceanic and Atmospheric Administration’s (NOAA’s) National Weather Service (NWS) were generally based on the Norwegian Cyclone Model (Bjerknes 1919) over land, and in recent decades, the Shapiro-Keyser Model over the mid-latitudes of the ocean. The graphic below shows a typical evolution according to both models of cyclone development. Conceptual models of cyclone evolution showing lower-tropospheric (e.g., 850-hPa) geopotential height and fronts (top), and lower-tropospheric potential temperature (bottom). (a) Norwegian cyclone model: (I) incipient frontal cyclone, (II) and (III) narrowing warm sector, (IV) occlusion; (b) Shapiro–Keyser cyclone model: (I) incipient frontal cyclone, (II) frontal fracture, (III) frontal T-bone and bent-back front, (IV) frontal T-bone and warm seclusion. Panel (b) is adapted from Shapiro and Keyser (1990) , their FIG. 10.27 ) to enhance the zonal elongation of the cyclone and fronts and to reflect the continued existence of the frontal T-bone in stage IV. -
Effect of Intense Wind Shear Across the Inversion on Stratocumulus Clouds
GEOPHYSICAL RESEARCH LETTERS, VOL. 35, L15814, doi:10.1029/2008GL033865, 2008 Click Here for Full Article Effect of intense wind shear across the inversion on stratocumulus clouds Shouping Wang,1 Jean-Christophe Golaz,2 and Qing Wang3 Received 17 March 2008; revised 12 May 2008; accepted 9 July 2008; published 13 August 2008. [1] A large-eddy simulation model is used to examine the mental difference between the strongly sheared and the impact of the intense cross-inversion wind shear on the shear-free stratocumulus convection? stratocumulus cloud structure. The wind shear enhanced [3] A low-level jet near the top of the CTBL is frequently entrainment mixing effectively reduces the cloud water and observed off the California central coast during summer due thickens the inversion layer. It leads to a reduction of the to the topography and land-sea contrast [Strom et al., 2001; turbulence kinetic energy (TKE) production in the cloud Rahn and Parish, 2007]. Figures 1a–1c show soundings layer due to the weakened cloud-top radiative cooling and taken in an aircraft flight in the field experiment of the formation of a turbulent and cloud free sublayer within Development and Evolution of Coastal Stratocumulus the inversion. The thickness of the sublayer increases with the [Kalogiros and Wang, 2002]. The wind speed reaches enhanced wind shear intensity. Under the condition of a maximum 18 msÀ1 just below the base of the inversion; weaker inversion, the enhanced shear mixing within the decreases by 8 msÀ1 across the sharp inversion; and then inversion layer even lowers the cloud-top height and reduces reduces further but more gradually to 7 m sÀ1 at about 730 m. -
Impact of Cloud Analysis on Numerical Weather Prediction in the Galician Region of Spain
Impact of Cloud Analysis on Numerical Weather Prediction in the Galician Region of Spain M. J. SOUTO, C. F. BALSEIRO AND V. P…REZ-MU—UZURI Group of Nonlinear Physics, Faculty of Physics, University of Santiago de Compostela, Santiago de Compostela, Spain Ming Xue University of Oklahoma, School of Meteorology, and CAPS Oklahoma, USA Keith BREWSTER Center for Analysis and Prediction of Storms, Oklahoma, USA April, 2001 Revised December, 2001 Corresponding author address: Dra. M. J. Souto, Group of Nonlinear Physics Faculty of Physics, University of Santiago de Compostela E-15706, Santiago de Compostela, Spain e-mail: [email protected] ABSTRACT The Advanced Regional Prediction System (ARPS) is applied to operational numerical weather forecast in Galicia, northwest Spain. A 72-hour forecast at a 10-km horizontal resolution is produced dta for the region. Located on the northwest coast of Spain and influenced by the Atlantic weather systems, Galicia has a high percentage (almost 50%) of rainy days per year. For these reasons, the precipitation processes and the initialization of moisture and cloud fields are very important. Even though the ARPS model has a sophisticated data analysis system (ADAS) that includes a 3D cloud analysis package, due to operational constraint, our current forecast starts from 12-hour forecast of the NCEP AVN model. Still, procedures from the ADAS cloud analysis are being used to construct the cloud fields based on AVN data, and then applied to initialize the microphysical variables in ARPS. Comparisons of the ARPS predictions with local observations show that ARPS can predict quite well both the daily total precipitation and its spatial distribution. -
Geography 5942 Synoptic Meteorology: Severe Storm Forecasting Spring 2017
Geography 5942 Synoptic Meteorology: Severe Storm Forecasting Spring 2017 Instructor: Jeff Rogers, Prof. Emeritus Office: Derby 1048 e-mail: [email protected] Phone: 292-0148 Office Hours: Tu, Th 2:10-3:30p.m. Course Prerequisites: Geography 5941, Physics 1250 Class Meetings: Tu, Th, 3:55 – 5:15 p.m. in Db 0140 Access to course lecture materials: http://carmen.osu.edu. Suggested Textbook: Mesoscale Meteorology in Midlatitudes by Paul Markowski and YvetteRichardson. Order through websites such as Amazon, it has not been ordered for the OSU bookstores. Course Objectives: The aim of the course is to introduce students to the methods of analysis and techniques of forecasting thunderstorms and severe weather. The course is divided into five components: 1. Introductory overview of the climatology of severe weather and basic cloud physics, 2. The meteorological ingredients for severe weather and the forecasting of severe weather, 3. Weather radar and satellites as tools in severe weather analysis, 4. Convection and the characteristics and features of mesoscale storms, and 5. Practice in severe weather forecasting through a series of exercises and assignments. The initial course section focuses on the ingredients of, and synoptic setting in which, severe storms develop. The role of instability, moisture, low-level and upper-level synoptic scale uplift will be described as will means by which forecasters identify and categorize the importance of each of these. The subsequent segment of the course describes the ways in which weather radar and geostationary satellite imagery are used in the analysis and forecasting of severe weather. Some theory of radar and satellite imagery is covered but the emphasis is on the usage of these materials in preparing forecasts and in trying to understand the conditions that are ideal for severe weather development. -
Emergency Procedures C172
EMERGENCY PROCEDURES NON CRITICAL ACTION June 2015 1. Maintain aircraft control. Table of Contents 2. Analyze the situation and take proper action. C 172 3.Land as soon as conditions permit NON CRITICAL ACTION PROCEDURES E-2 GROUND OPERATION EMERGENCIES GROUND OPERATION EMERGENCIES E-2 Emergency Engine Shutdown on the Ground Emergency Engine Shutdown on the Ground E-2 1. FUEL SELECTOR -------------------------------- OFF Engine Fire During Start E-2 2. MIXTURE ---------------------------- IDLE CUTOFF TAKEOFF EMERGENCIES E-2 3. IGNITION ------------------------------------------ OFF Abort E-2 4. MASTER SWITCH ------------------------------- OFF IN-FLIGHT EMERGENCIES E-3 Engine Failure Immediately After T/O E-3 Engine Fire during Start Engine Failure In Flt - Forced Landing E-3 If Engine starts Engine Fire During Flight E-4 1. POWER ------------------------------------- 1700 RPM Emergency Descent E-4 2. ENGINE -------------------------------- SHUTDOWN Electrical Fire/High Ammeter E-4 If Engine fails to start Negative Ammeter Reading E-4 1. CRANKING ----------------------------- CONTINUE Smoke and Fume Elimination E-5 2. MIXTURE --------------------------- IDLE CUT-OFF Oil System Malfunction E-4 3 THROTTLE ----------------------------- FULL OPEN Structural Damage or Controllability Check E-5 4. ENGINE -------------------------------- SHUTDOWN Recall E-6 FUEL SELECTOR ------ OFF Lost Procedures E-6 IGNITION SWITCH --- OFF Radio Failure E-7 MASTER SWITCH ----- OFF Diversions E-8 LANDING EMERGENCIES E-9 TAKEOFF EMERGENCIES Landing with flat tire E-9 ABORT E-9 LIGHT SIGNALS 1. THROTTLE -------------------------------------- IDLE 2. BRAKES ----------------------------- AS REQUIRED E-2 E-1 IN-FLIGHT EMERGENCIES Engine Fire During Flight Engine Failure Immediately After Takeoff 1. FUEL SELECTOR --------------------------------------- OFF 1. BEST GLIDE ------------------------------------ ESTABLISH 2. MIXTURE------------------------------------ IDLE CUTOFF 2. FUEL SELECTOR ----------------------------------------- OFF 3. -
ESSENTIALS of METEOROLOGY (7Th Ed.) GLOSSARY
ESSENTIALS OF METEOROLOGY (7th ed.) GLOSSARY Chapter 1 Aerosols Tiny suspended solid particles (dust, smoke, etc.) or liquid droplets that enter the atmosphere from either natural or human (anthropogenic) sources, such as the burning of fossil fuels. Sulfur-containing fossil fuels, such as coal, produce sulfate aerosols. Air density The ratio of the mass of a substance to the volume occupied by it. Air density is usually expressed as g/cm3 or kg/m3. Also See Density. Air pressure The pressure exerted by the mass of air above a given point, usually expressed in millibars (mb), inches of (atmospheric mercury (Hg) or in hectopascals (hPa). pressure) Atmosphere The envelope of gases that surround a planet and are held to it by the planet's gravitational attraction. The earth's atmosphere is mainly nitrogen and oxygen. Carbon dioxide (CO2) A colorless, odorless gas whose concentration is about 0.039 percent (390 ppm) in a volume of air near sea level. It is a selective absorber of infrared radiation and, consequently, it is important in the earth's atmospheric greenhouse effect. Solid CO2 is called dry ice. Climate The accumulation of daily and seasonal weather events over a long period of time. Front The transition zone between two distinct air masses. Hurricane A tropical cyclone having winds in excess of 64 knots (74 mi/hr). Ionosphere An electrified region of the upper atmosphere where fairly large concentrations of ions and free electrons exist. Lapse rate The rate at which an atmospheric variable (usually temperature) decreases with height. (See Environmental lapse rate.) Mesosphere The atmospheric layer between the stratosphere and the thermosphere. -
Severe Weather Forecasting Tip Sheet: WFO Louisville
Severe Weather Forecasting Tip Sheet: WFO Louisville Vertical Wind Shear & SRH Tornadic Supercells 0-6 km bulk shear > 40 kts – supercells Unstable warm sector air mass, with well-defined warm and cold fronts (i.e., strong extratropical cyclone) 0-6 km bulk shear 20-35 kts – organized multicells Strong mid and upper-level jet observed to dive southward into upper-level shortwave trough, then 0-6 km bulk shear < 10-20 kts – disorganized multicells rapidly exit the trough and cross into the warm sector air mass. 0-8 km bulk shear > 52 kts – long-lived supercells Pronounced upper-level divergence occurs on the nose and exit region of the jet. 0-3 km bulk shear > 30-40 kts – bowing thunderstorms A low-level jet forms in response to upper-level jet, which increases northward flux of moisture. SRH Intense northwest-southwest upper-level flow/strong southerly low-level flow creates a wind profile which 0-3 km SRH > 150 m2 s-2 = updraft rotation becomes more likely 2 -2 is very conducive for supercell development. Storms often exhibit rapid development along cold front, 0-3 km SRH > 300-400 m s = rotating updrafts and supercell development likely dryline, or pre-frontal convergence axis, and then move east into warm sector. BOTH 2 -2 Most intense tornadic supercells often occur in close proximity to where upper-level jet intersects low- 0-6 km shear < 35 kts with 0-3 km SRH > 150 m s – brief rotation but not persistent level jet, although tornadic supercells can occur north and south of upper jet as well.