High Speed Rail Tunnel Aerodynamics: Transient pressure and loadings on fixed tunnel equipment

Similar documents
AIRFLOW GENERATION IN A TUNNEL USING A SACCARDO VENTILATION SYSTEM AGAINST THE BUOYANCY EFFECT PRODUCED BY A FIRE

AN INVESTIGATION OF LONGITUDINAL VENTILATION FOR SHORT ROAD TUNNELS WITH HIGH FIRE HRR

METRO System Design. Witt&Sohn AG Aug-11

NUMERICAL INVESTIGATION OF THE FLOW BEHAVIOUR IN A MODERN TRAFFIC TUNNEL IN CASE OF FIRE INCIDENT

A STUDY OF THE LOSSES AND INTERACTIONS BETWEEN ONE OR MORE BOW THRUSTERS AND A CATAMARAN HULL

OPTIMIZING THE LENGTH OF AIR SUPPLY DUCT IN CROSS CONNECTIONS OF GOTTHARD BASE TUNNEL. Rehan Yousaf 1, Oliver Scherer 1

Sizing of extraction ventilation system and air leakage calculations for SR99 tunnel fire scenarios

Preliminary design of a high-altitude kite. A flexible membrane kite section at various wind speeds

Measurements of the effect on pressures of a porous tunnel entrance using a moving model rig.

An Impeller Blade Analysis of Centrifugal Gas Compressor Using CFD

Autodesk Moldflow Communicator Process settings

The Usage of Propeller Tunnels For Higher Efficiency and Lower Vibration. M. Burak Şamşul

Safety, ventilation and climate in rail tunnels

Wave Load Pattern Definition

CONSIDERATION OF DENSITY VARIATIONS IN THE DESIGN OF A VENTILATION SYSTEM FOR ROAD TUNNELS

Special edition paper

PIG MOTION AND DYNAMICS IN COMPLEX GAS NETWORKS. Dr Aidan O Donoghue, Pipeline Research Limited, Glasgow

Research on Small Wind Power System Based on H-type Vertical Wind Turbine Rong-Qiang GUAN a, Jing YU b

MODELLING OF FUME EXTRACTORS C. R.

Courses of Instruction: Controlling and Monitoring of Pipelines

THE IMPACT OF PRESSURE AND SUCTION WAVES ON INSTALLED COMPONENTS, WITH PARTICULAR REFERENCE TO ENCLOSURES IN RAILWAY TUNNELS

Lab # 03: Visualization of Shock Waves by using Schlieren Technique

OPTIMIZATION OF SINGLE STAGE AXIAL FLOW COMPRESSOR FOR DIFFERENT ROTATIONAL SPEED USING CFD

Forest Winds in Complex Terrain

Learn more at

ZIN Technologies PHi Engineering Support. PHi-RPT CFD Analysis of Large Bubble Mixing. June 26, 2006

Tutorial. BOSfluids. Relief valve

THEORETICAL EVALUATION OF FLOW THROUGH CENTRIFUGAL COMPRESSOR STAGE

AUSTRIAN RISK ANALYSIS FOR ROAD TUNNELS Development of a new Method for the Risk Assessment of Road Tunnels

Ermenek Dam and HEPP: Spillway Test & 3D Numeric-Hydraulic Analysis of Jet Collision

2001 AASHTO Training Manual

Pedestrian traffic flow operations on a platform: observations and comparison with simulation tool SimPed

Transient Analyses In Relief Systems

CFD ANALYSIS AND COMPARISON USING ANSYS AND STAR-CCM+ OF MODEL AEROFOIL SELIG 1223

IMO REVISION OF THE INTACT STABILITY CODE. Proposal of methodology of direct assessment for stability under dead ship condition. Submitted by Japan

ROSE-HULMAN INSTITUTE OF TECHNOLOGY Department of Mechanical Engineering. Mini-project 3 Tennis ball launcher

INTERACTION BETWEEN WIND-DRIVEN AND BUOYANCY-DRIVEN NATURAL VENTILATION Bo Wang, Foster and Partners, London, UK

UNIT 15 WATER HAMMER AND SURGE TANKS

I.CHEM.E. SYMPOSIUM SERIES NO. 97 BUOYANCY-DRIVEN NATURAL VENTILATION OP ENCLOSED SPACES

RESEARCH OF BLOCKAGE SEGMENT DETECTION IN WATER SUPPLY PIPELINE BASED ON FLUID TRANSIENT ANALYSIS ABSTRACT

A Study on Roll Damping of Bilge Keels for New Non-Ballast Ship with Rounder Cross Section

6. EXPERIMENTAL METHOD. A primary result of the current research effort is the design of an experimental

ANALYSIS OF AERODYNAMIC CHARACTERISTICS OF A SUPERCRITICAL AIRFOIL FOR LOW SPEED AIRCRAFT

EXPERIMENTAL STUDY ON THE DISCHARGE CHARACTERISTICS OF SLUICE FOR TIDAL POWER PLANT

Evaluation of the optimum conditions for a local ventilation system in connection with the mine ventilation network

Ship Resistance and Propulsion Prof. Dr. P. Krishnankutty Ocean Department Indian Institute of Technology, Madras

Head Impact Analysis Validation for Aluminium Bonnet

SUBPART C - STRUCTURE

Fire and Safety for Offshore drilling and production Ajey Walavalkar ANSYS Inc.

Understanding the Factors Governing Motorsport Safety Fence Design Through DOE Techniques. In conjunction with the GRM. Andrew Mellor Joe Johnson

LONGITUDINAL AIR VELOCITY CONTROL IN A ROAD TUNNEL DURING A FIRE EVENT

Evaluating and Preventing Capacity Loss when Designing Train Control to Enforce NFPA 130 Compliance

SEMI-SPAN TESTING IN WIND TUNNELS

Influence of rounding corners on unsteady flow and heat transfer around a square cylinder

Aalborg Universitet. Published in: Proceedings of Offshore Wind 2007 Conference & Exhibition. Publication date: 2007

II.E. Airplane Flight Controls

Effect of Inlet Clearance Gap on the Performance of an Industrial Centrifugal Blower with Parallel Wall Volute

Sizing Pulsation Dampeners Is Critical to Effectiveness

OIL AND GAS INDUSTRY

E02 Rigid hinged stinger with piggyback line

Write important assumptions used in derivation of Bernoulli s equation. Apart from an airplane wing, give an example based on Bernoulli s principle

Start-up of the Three-shaft Closed Loop

THE EFFECT OF HEEL ANGLE AND FREE-SURFACE PROXIMITY ON THE PERFORMANCE AND STRUT WAKE OF A MOTH SAILING DINGHY RUDDER T-FOIL

Lehigh-FIU Hybrid Wind Simulation Developments

Improvement of the Volumetric and Isentropic Efficiency Due to Modifications of the Suction Chamber

CFD Analysis of Giromill Type Vertical Axis Wind Turbine

OPTIMISATION OF VENTILATION IN THE CASE OF A FIRE IN ROAD TUNNELS

S-CO 2 Brayton Recompression Loop Design and Control

Smoke and heat Ventilator Testing

MODELING&SIMULATION EXTRAPOLATED INTERNAL ARC TEST RESULTS: A COUPLED FLUID-STRUCTURAL TRANSIENT METHODOLOGY

6.6 Gradually Varied Flow

Fire safety of staircases in multi-storey buildings The results of measurements in Buildings and Simulations

Quantitative risk assessment and risk-based decision making

PRAGMATIC ASSESSMENT OF EXPLOSION RISKS TO THE CONTROL ROOM BUILDING OF A VINYL CHLORIDE PLANT

Tools for safety management Effectiveness of risk mitigation measures. Bernhard KOHL

Development of TEU Type Mega Container Carrier

Investigation of Suction Process of Scroll Compressors

CFD SIMULATIONS OF GAS DISPERSION IN VENTILATED ROOMS

Wave Motion. interference destructive interferecne constructive interference in phase. out of phase standing wave antinodes resonant frequencies

RESIDENTIAL WATER DISTRIBUTION

Experimental Characterization and Modeling of Helium Dispersion in a ¼-Scale Two-Car Residential Garage

ASSESSMENT AND ANALYSIS OF PIPELINE BUCKLES

Numerical and Experimental Analysis of the Pressure Signature for different High-Speed Trains

LOW PRESSURE EFFUSION OF GASES adapted by Luke Hanley and Mike Trenary

Figure 1. The distance the train travels between A and B is not the same as the displacement of the train.

JAR-23 Normal, Utility, Aerobatic, and Commuter Category Aeroplanes \ Issued 11 March 1994 \ Section 1- Requirements \ Subpart C - Structure \ General

Waves. harmonic wave wave equation one dimensional wave equation principle of wave fronts plane waves law of reflection

Conventional Ship Testing

A Chiller Control Algorithm for Multiple Variablespeed Centrifugal Compressors

No Description Direction Source 1. Thrust

Flow in a shock tube

Efficiency Improvement of Rotary Compressor by Improving the Discharge path through Simulation

Khosla's theory. After studying a lot of dam failure constructed based on Bligh s theory, Khosla came out with the following;

Hydrostatic Force on a Submerged Surface

SHOT ON GOAL. Name: Football scoring a goal and trigonometry Ian Edwards Luther College Teachers Teaching with Technology

Friction properties of the face of a hand-held tennis racket

PRESSURE SURGES IN PIPELINES

Appendix FRANCE Lyon Croix-Rousse Tunnel

Characteristics of Decompression Tank Internally Pressurized With Water Using OpenFOAM Syamsuri 1, a

Inlet Swirl on Turbocharger Compressor Performance

Transcription:

High Speed Rail Tunnel Aerodynamics: Transient pressure and loadings on fixed tunnel equipment Mohammad Tabarra & Richard Sturt Arup, UK Summary: Trains entering tunnels at high speeds can generate highly transient air velocity and pressure fields inside the tunnel, from time of entry until well after they leave the tunnel. The parameters affecting the induced velocity and pressure fields include train speed, train to tunnel blockage ratio, train to tunnel length ratio, shape of train nose and tail, and the number, spacing intervals and area of pressure relief shafts. Compression waves induced by the train nose and tail propagate along the tunnel at the speed of sound, and compress and accelerate air in front of it, until they reach the exit portal. These will then reflect as refraction waves, interact with other travelling waves and set up complex wave patterns and airflows. Some of the rapid pressure changes can create aural discomfort for passengers. The designer has to ensure that the cross sectional area of the tunnel is large enough so as not to exceed these maximum pressure thresholds. In cases where the required tunnel cross section cannot be met, other engineering solutions like the provision of pressure relief shafts are considered. Apart from provision of pressure relief, a separate mechanical ventilation system is needed to provide a safe environment during an emergency fire incident, as well as a comfort for passengers in a train congestion scenario. While large axial fans in supply and extract configuration have been the traditional solution, other approaches are possible like Saccardo nozzles and jet fans, as used in the Channel Tunnel Rail Link (HS1). Thus the issue of transient forces and moments on installed equipment such as fans, signs, brackets and panels in high-speed tunnels are discussed, drawing on the experience of HS1.. Index Terms: high speed rail tunnel aerodynamics, transient pressure, transient loads on fixed equipment 1. BACKGROUND When a train passes through a tunnel it induces pressure waves which travel up and down the tunnel at the speed of sound, passing over any trains in the tunnel and causing the pressure inside the trains to fluctuate. These variations in pressure are experienced by passengers and can manifest themselves as discomfort in the inner ear. If the train is sealed, the pressure inside the train will be different from the pressure outside the train. The inside pressures are used to assess comfort criteria, while the outside pressures are used for the TSI criteria (Technical Standard for Interoperability limit 10kPa), mandated in Europe. These pressure fields need to be predicted by designers, to allow for adequate pressure relief during normal train operations, under a variety of train speeds. The impact of rapidly changing pressure and velocity fields on fixed equipment and the resulting forces and moments have to be assessed, to ensure safe operation of the railway. These loads have to be considered both from a fatigue point of view, as well as a peak maximum magnitude. The aim of this paper is twofold; first it presents the results of a methodology of sizing high-speed

tunnels for a range of train and tunnel configurations, and to discuss the impacts on rail infrastructure planning, as far as rail tunnels are concerned. In addition, it shares the experience gained during design to predict transient loads (forces and moments) on tunnel fixed equipment in an existing high-speed single-track tunnel. 2. PRESSURE SIMULATIONS 2.1 Computer simulation code: Arup developed TunX as a one-dimensional finite difference code for predicting pressure transients for a variety of trains and tunnel configurations. The formation and propagation of these waves are unsteady thermodynamic processes which can be described by equations representing Newton s Second Law, the conservation of mass and momentum and isentropic flow. TunX solves these equations numerically in a timestepping manner. The tunnel network (including vent shafts and cross passages) is first divided into a number of elements of equal length through which air and trains can pass. Losses at portals, vent shafts, noses and tails of trains etc. are represented by pressure loss coefficients. For sealed trains, further elements inside the train connect to the air outside the train via holes with a user-specified time-constant representing the efficacy of sealing. To find the optimum tunnel area to pass a given pressure comfort criterion, a purpose-written optimiser known as MultiTunX performs multiple runs of TunX automatically. The tunnel area is treated as a design variable to be optimised. The automatic process can be extended to be applied to, for example, a list of tunnel lengths or train speeds. For two trains running in opposite directions through a 2-track tunnel, simultaneous entry of the trains is not necessarily the worst case. MultiTunX tries a range of time-offsets and finds the optimum tunnel area that passes the comfort criteria for all time-offsets. 2.2 Code validation Tunx has been validated against predictions and measured data and predictions, and against measurements carried out by Arup in a UK tunnel during 2001. Figure 1 presents examples of measured and predicted traces of pressure transients at 80m from the south portal for a Class 91 train entering a tunnel at a speed of 104 mph (167 kph). Figure 1: Measured versus predicted pressure transients

2.3 Scenarios The scenarios modeled assumes a 200 m long streamlined high speed train, with a cross sectional area of 11m 2 sealed with time-constant 10sec, entering a tunnel at a speed of 350 kph. The sample tunnel length is 1.6km, and the pressure criteria to comply with are both: TSI (<10kPa pressure change in whole event) UIC 2005 baseline pressure comfort criteria (1kPa/1sec, 1.6kPa/4sec, 2kPa/10sec) The objective is to optimise the tunnel crosssectional area to meet comfort criterion exactly, with and without pressure relief shafts. Note that the height of tunnel, train, and dimensions of shaft are exaggerated in these plots for clarity. The addition of a pressure relief shaft breaks up the pressure waves; the changes of pressure become smaller but more numerous. Figure 3 illustrates pressure at a point near the rear of the train, outside the train s sealing system, with and without pressure relief shaft. The set of simulations begin with a single train entering a single track tunnel, and then continues to the case of two trains entering a two-track tunnel in opposite directions at different time intervals. 2.4 Single track tunnels 2.4.1 Pressure transients The first set of simulations focus on a single train entering the tunnel, and the cross-sectional area is optimised to meet comfort criterion exactly, without pressure relief shafts. The simulation is then run again with one or more pressure relief shafts. Figure 2 illustrates the range of positive and negative pressures induced with and without the pressure relief shaft. Figure 3: Pressure variations with time outside the train, with and without a relief shaft To assess the effect on aural comfort, consider the pressure inside the sealed train. Without pressure relief shafts, the comfort criterion 2kPa / 10sec is met exactly. This is shown in Figure 4, whereas with a pressure relief shaft, the maximum pressure change in 10 sec is reduced to 1.3kPa (36% reduction). This illustrates the positive impact of a pressure relief shaft on the rate of pressure change, to which the human ear is most sensitive. Figure 2: Still image of pressure waves from a single train with and without a relief shaft

Figure 4: Pressure variations with time inside a single train with and without a relief shaft Figure 5: The impact of pressure relief shafts on the optimum cross sectional area of a tunnel single train @ 350 kph 2.4.2 Tunnel area optimization This section shows the result of optimising the tunnel area to meet the comfort criteria (and also ensure that the TSI is met), for different tunnel lengths and different numbers of pressure relief shafts. The pressure relief shafts are positioned in each case such that the tunnel is divided into equal lengths. Each point on the graph is the result of a set of optimisation calculations. The optimisation calculations are performed and repeated automatically for different tunnel lengths. In this particular exercise, for different tunnel lengths, the impact of one, two or three pressure relief shafts are assessed for a given single train passing at a speed of 350 kph. Figure 5 shows that in the example modelled, a 1.6 km tunnel needs a cross-sectional area 67.5 m 2 without relief shafts, or 47.5 m 2 with one relief shaft, to meet the comfort criteria. The fluctuations of required tunnel area observed are a result of wave harmonics and are a function of tunnel to train length ratio. Alternatively the effect of train speed on the free cross sectional area of a single track tunnel can be studied. This is of particular interest to train operators who wish to reduce journey times, and therefore wish to raise the line speed of their train operations on long distance services Figure 6 illustrates the increase in tunnel cross section needed to accommodate higher train speeds, without causing aural discomfort. For example a 3 km tunnel with a 48 m 2 free cross sectional area and one relief shaft can accommodate a 300 kph train speed, but would need to be enlarged to 75 m 2 to provide the minimum required passenger aural comfort for a 400 kph train service. This kind of information is extremely valuable at the initial stages of rail infrastructure planning when tunnels are being designed and built, as later changes and enlargements to tunnel structure will not be feasible.

operating trains in double track tunnels will require a 30-40% larger area for a 400 kph train speed, compared to 350 kph. In many infrastructure projects, this can be a large price to pay for reduced journey times, and a cost-benefit analysis becomes mandatory in the initial infrastructure planning stages. Figure 6: The impact of train speed on the optimum cross sectional area of a single-track tunnel 2.5 Two-track tunnels 2.5.1 Pressure transients The pressure transient simulations are repeated for a two-track tunnel with and without pressure relief shafts for trains entering the tunnel in opposite directions at different time intervals. 2.5.2 Tunnel area optimization The same tunnel sizing exercise is repeated for various lengths of a two-track tunnel with one pressure relief shaft at two train speeds. The code optimizes the tunnel size to cope with any combination of train entry-times; so for each tunnel length, about 30 different cases are checked to find a tunnel size that fulfils the aural comfort criteria for all those combinations. In total, each line on the graph takes over 1000 separate analyses, all done automatically. Figure 7 shows the impact of train speed on free cross sectional area required to comply with the passenger aural comfort criteria. It can be seen that Figure 7: The impact of train speed on the optimum cross sectional area of a two-track tunnel 3. TRANSIENT LOADS ON EQUIPMENT 3.1 HS1 tunnel In this section, transient forces and moments on fixed tunnel equipment such as signs, cables, wayside boxes in a typical high-speed single-track rail tunnel is presented. While the study focuses on tunnels on the Channel Tunnel Rail Link (HS1) route (Dover to London), general conclusions can be extended to other high-speed rail tunnels. The pressure wave associated with the train nose has a strong peak generating a highly transient longitudinal and lateral velocity field in the tunnel. This velocity (as distinct from the pressure wave) impacts the electrical and mechanical equipment and systems installed on the tunnel walls and ceilings jet fans, signal boards, cable trays, fire

pipes, leaky feeders, cross passage doors, etc, as seen in Figure 8. Every time a train enters and passes through the tunnel, there are five distinct stages of flow development leading to a time-varying velocity and pressure field, as viewed by a piece of equipment fixed to the tunnel walls at any position along the tunnel: 1) Longitudinal piston effect plug flow in front of the approaching train 2) Short duration load as the train nose arrives 3) Longer duration longitudinal flow in the train/tunnel annulus as the body of the train passes the fixed equipment 4) Short duration load as the train tail end passes 5) Longitudinal piston effect plug flow in the trail of the departing train (same as 1) The flow conditions for stages 1 and 5 are similar due to flow continuity requirements; hence the loads on the fixed equipment will also be similar, so only one needs to be considered. Stages 2 and 4 generate a short velocity and pressure wave pulse, but the loads due to the passage of train tail end are in the reverse direction and smaller in magnitude compared to the loads during the passage of train nose. Hence stage 4 loads will not be considered any further, as stage 2 loads, when reversed in direction, adequately cover them. Furthermore the complexity of the case may be reduced by making the artificial assumption that there is an infinite resistance ahead of the train and thus there will be no piston effect flow at all, leading to 100% flow reversal over the train. While this is a very conservative approach, it eliminates the loads in stages 1 and 5 above, but accentuates the loads in stage 3. Since the flow in stage 3 represents higher air velocities anyway, with higher drag and skin friction forces, this conservative approach is recommended. Therefore among the various stages of flow development, stages 2 and 3 are expected to contain the highest longitudinal, transverse and vertical forces and moments exerted on the tunnel fixed equipment. Hence only stages 2 and 3 flow scenarios need to be investigated in depth in order to estimate the maximum loading encountered and inform the design of the mounting brackets. Note that the pressure wave (as distinct from the air velocity) travelling with the train nose does not normally affect equipment that has a short length in the direction of tunnel axis and is fully submerged in tunnel air, as the overall pressure force is zero; it only affects equipment partially exposed to the tunnel air (experiences an unbalanced short pulse transverse force, like a poster attached to the wall) or equipment which has a significant finite dimension in the direction of tunnel length and end surfaces (experiences different points of the pressure wave at any one time and hence an unbalanced short pulse longitudinal force). Table 1 and 2 present the basic HS1 train and tunnel data, as well as the tunnel fixed equipment. Figure 8: HS1 tunnel section (courtesy of RLE)

Table 1 Tunnel and Train Basic Data Parameter Tunnel int. diameter single track Value 7150 mm Tunnel full cross sectional area 36.5 m² Train speed in tunnel 230 kph Train cross section area 9.5 m² Y Tunnel/train annulus section area 27 m² Table 2 Tunnel Fixed Equipment Selected for the Aerodynamic Loading Analysis Tunnel fixed equipment Size (mm) Figure 9. Frame of reference for HS1 tunnel X Z Signalling Location Case Transformer (TAD) Tunnel Marker Post Leaky Feeder Cable 820H x 470W x 820L 220H x 90W x 360L 480H x 560W x 0L 32 diameter 3.2 Methodology The aim was to estimate the maximum loads experienced by selected fixed equipment due to passing trains in a single-track tunnel. Two approaches were adopted for the derivation of aerodynamic loads and results compared: a) An independent first-order engineering desk study (e.g, slender body theory) estimating the likely velocity fields and the resulting forces and moments on tunnel fixed equipment that accompany the movement of the high speed train in the tunnel. b) An interpretation of the CFD results of the velocity and pressure fields and the forces and moments. The CFD graphical results (CFX5) were used for this approach, and extrapolated to selected equipment with different dimensions, as shown in Table 2. Note all forces, moments and air velocities are discussed in the x-y-z axes with z-axis along the tunnel, x-axis horizontal transverse, and y-axis vertical, as seen in Figure 9. Of the four selected pieces of equipment, two were not directly affected by the pressure wave transients, as they are fully immersed in tunnel environment and have a short length. The leaky feeder is a continuous cable and has no end surface to be affected by pressure differential forces. The tunnel marker posts are also very short in length (in the z-direction, along the tunnel), and hence will not experience pressure differentials. So only the signalling location case and the TAD box will experience longitudinal forces due to the pressure wave of stages 2 and 4. 3.3 Results Results of the first-order engineering desk study and CFD are shown in Tables 3 to 6, where forces and moments on all 3 axes are shown for each of the four pieces of tunnel fixed equipment.

Table 3. Forces on Fixed Equipment (desk study) Tunnel Fixed Equipment F x (N) F y (N) F z (N) Signalling Location Case 363 / 0 229 / 0 180 / 130 TAD Box 47 / 0 19 / 0 6 / 7 Tunnel Marker Post 0 / 0 0 / 0 63 / 115 Leaky Feeder Cable 30 / 0 30 / 0 0 / 0 Table 4. Moments on Fixed Equipment (desk study) Tunnel Fixed Equipment M x (Nm) M y (Nm) M z (Nm) Signalling Location Case 168 / 0 191 / 69 203 / 0 TAD Box 4 / 0 9 / 0.7 6 / 0 Tunnel Marker Post 15 / 28 18 / 32 0 / 0 Leaky Feeder Cable 20 / 0 20 / 0 0 / 0 Table 5. Forces on Fixed Equipment (CFD) Tunnel Fixed Equipment F x (N) F y (N) F z (N) Signalling Location Case 129 / 25 71 / 4 95 / 149 TAD Box 16 / 3 6 / 3 2 / 8 Tunnel Marker Post 0 / 0 0 / 0 68 / 87 Leaky Feeder Cable 3 / 0 5 / 0 0.4 / 0.3 Table 6. Moments on Fixed Equipment (CFD) Tunnel Fixed Equipment M x (Nm) M y (Nm) M z (Nm) Signalling Location Case 55 / 3 145 / 0.3 0 / 0 TAD Box 5 / 0.25 17 / 0.03 0 / 0 Tunnel Marker Post N/A / N/A N/A / N/A 0 / 0 Leaky Feeder Cable 22 / 0 18 / 0 0 / 0 It can be seen that the forces and moment estimates from the desk study were higher than the CFD analysis, which was expected, as conservative estimates of air velocity were made in the stage 3. Note these forces and moments will be applied cyclically with every train passage, so a fatigue design approach (e.g. S-N curve, fatigue strength versus number of stress cycles) would be needed for the support brackets of the fixed equipment. Assuming a train schedule of 5 trains per hour, operating for 20 hrs a day, over a 25-year design life of the tunnel systems, the support brackets would experience more than a million cycles, as some of the load peaks occur more than once for each train passage. Hence the infinite life portion of the S-N curves (N above 10 6 ) would form the design specification for the bracket manufacturer. It was thus recommended that the higher of the two figures quoted for the forces and moments be adopted for design to provide a margin of safety, even though some of the CFD extrapolated figures may be closer to reality. 4. CONCLUSIONS The pressure transients induced by a high speed train entering a tunnel have a very significant impact on the free cross section of the tunnel at initial planning stages. Achieving the aural comfort of passengers is the key criterion for dimensioning tunnels and/or pressure relief shafts, for a given set of train speed, area and length. Increasing train speeds will be limited by existing tunnel size, even if the rolling stock is capable of higher speeds. Separately, the rapidly varying velocity fields around the approaching train will impart drag forces and moments on tunnel fixed equipment along all three axes. Typical loads are shown for a single-track tunnel and have informed the fatigue design of brackets and fixtures to tunnel walls. Acknowledgements The authors would like to thank Rail Link Engineering (RLE) for access to HS1 data.