DESIGN AND CHARACTERISATION OF A DOUBLE-PISTON PRESSURE BALANCE IN HIGH PRESSURE

Similar documents
An Innovative Solution for Water Bottling Using PET

A New Piston Gauge to Improve the Definition of High Gas Pressure and to Facilitate the Gas to Oil Transition in a Pressure Calibration Chain

Investigation of Stresses in Ring Stiffened Circular Cylinder

Organisation Internationale de Métrologie Légale

XIX IMEKO World Congress Fundamental and Applied Metrology September 6 11, 2009, Lisbon, Portugal

Modeling of thin strip profile during cold rolling on roll crossing and shifting mill

Calibration methods for negative gauge pressure down to -100 kpa

WATER HYDRAULIC HIGH SPEED SOLENOID VALVE AND ITS APPLICATION

Analysis of dilatometer test in calibration chamber

Numerical analysis of influence of streamline rudder on screw propeller efficiency

FPG8601 Force Balanced Piston Gauge

machine design, Vol.6(2014) No.3, ISSN pp

Numerical analysis of gas leakage in the pistoncylinder clearance of reciprocating compressors considering compressibility effects

Numerical simulation of an intermediate sized bubble rising in a vertical pipe

Figure 1 Schematic of opposing air bearing concept

Pneumatic dead-weight tester Model CPB3500

Tightening Evaluation of New 400A Size Metal Gasket

Primary standard differential pressure balance Model CPB6000DP

Plastic non-symmetric bifurcation buckling of circular cylinders under uniform external hydrostatic pressure

Hydraulic pressure balance Model CPB5800

P3000 Series. Pneumatic Deadweight Testers Model P3000. Technical Data. Features

Analyses of the fuel cell stack assembly pressure

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

Study on the Influencing Factors of Gas Mixing Length in Nitrogen Displacement of Gas Pipeline Kun Huang 1,a Yan Xian 2,b Kunrong Shen 3,c

Safety Systems Based on ND Pressure Monitoring

Impact of imperfect sealing on the flow measurement of natural gas by orifice plates

An innovative technology for Coriolis metering under entrained gas conditions

Linear Compressor Discharge Manifold Design For High Thermal Efficiency

Numerical Simulation of Fluid-Structure Interaction in the Design Process for a New Axial Hydraulic Pump

International Journal of Modern Trends in Engineering and Research e-issn No.: , Date: 2-4 July, 2015

Investigation on 3-D Wing of commercial Aeroplane with Aerofoil NACA 2415 Using CFD Fluent

P3000 Series. Pneumatic Deadweight Testers Model P3000. Technical Data. Features

WIND-INDUCED LOADS OVER DOUBLE CANTILEVER BRIDGES UNDER CONSTRUCTION

PRESSURE DISTRIBUTION OF SMALL WIND TURBINE BLADE WITH WINGLETS ON ROTATING CONDITION USING WIND TUNNEL

DESIGN AND PERFORMANCE OF THE NEW SARTORIUS 1 KG VACUUM MASS COMPARATOR AT PTB

EFFECT OF CORNER CUTOFFS ON FLOW CHARACTERISTICS AROUND A SQUARE CYLINDER

STIFFNESS INVESTIGATION OF PNEUMATIC CYLINDERS. A. Czmerk, A. Bojtos ABSTRACT

LOW PRESSURE EFFUSION OF GASES revised by Igor Bolotin 03/05/12

STRESS ANALYSIS OF BELL CRANK LEVER

EXPERIMENTAL STUDY ON THE HYDRODYNAMIC BEHAVIORS OF TWO CONCENTRIC CYLINDERS

The Estimation Of Compressor Performance Using A Theoretical Analysis Of The Gas Flow Through the Muffler Combined With Valve Motion

AE Dept., KFUPM. Dr. Abdullah M. Al-Garni. Fuel Economy. Emissions Maximum Speed Acceleration Directional Stability Stability.

Numerical simulation and analysis of aerodynamic drag on a subsonic train in evacuated tube transportation

Analysis of hazard to operator during design process of safe ship power plant

Experimental Investigation Of Flow Past A Rough Surfaced Cylinder

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

Vertical Uplift Capacity of a Group of Equally Spaced Helical Screw Anchors in Sand

Validation of Custody Transfer Metering Skid at Site After Laboratory Proving

CHAPTER IV FINITE ELEMENT ANALYSIS OF THE KNEE JOINT WITHOUT A MEDICAL IMPLANT

Simulation and Experimentation on the Contact Width of New Metal Gasket for Asbestos Substitution

Micro Channel Recuperator for a Reverse Brayton Cycle Cryocooler

Axial and Radial Force Control for CO2 Scroll Expander

Using PV Diagram Synchronized With the Valve Functioning to Increase the Efficiency on the Reciprocating Hermetic Compressors

Guide for the uncertainty analysis in pressure when using P3000 Series Deadweight Testers

Chapter 4: Single Vertical Arch

THE IMPLEMENTATION OF TOROIDAL THROAT VENTURI NOZZLES TO MAXIMIZE PRECISION IN GAS FLOW TRANSFER STANDARD APPLICATIONS

PHYSICAL AND NUMERICAL MODELLING OF WAVE FIELD IN FRONT OF THE CONTAINER TERMINAL PEAR - PORT OF RIJEKA (ADRIATIC SEA)

3 1 PRESSURE. This is illustrated in Fig. 3 3.

Chapter 4. Tribology. 1. Lubrication. 2. Wear

THE PRESSURE SIGNAL CALIBRATION TECHNOLOGY OF THE COMPREHENSIVE TEST

Kazuhiko TOSHIMITSU 1, Hironori KIKUGAWA 2, Kohei SATO 3 and Takuya SATO 4. Introduction. Experimental Apparatus

EFFECTS OF BAFFLE SIZE ON PRESSURE DISTRIBUTION IN VACUUM CHAMBER DURING DYNAMIC GAS FLOW

A parametric study of metal-to-metal contact flanges with optimised. geometry for safe stress and no-leak conditions

Copyright by Turbomachinery Laboratory, Texas A&M University

CHARACTERISTICS OF LEAK DETECTION BASED ON DIFERENTIAL PRESSURE MEASUREMENT

PG7000 high line differential mode for defining differential pressure at line pressures above atmospheric pressure (PG7000 V2.

AIAA Brush Seal Performance Evaluation. P. F. Crudgington Cross Manufacturing Co. Ltd. Devizes, ENGLAND

Návrh vratného kanálu u dvoustupňového kompresoru Return channel design of the two stage compressor

Wind turbine Varying blade length with wind speed

STRIP EDGE SHAPE CONTROL

Pressure calibration equipment

Modeling of Gas Leakage through Compressor Valves

67. Sectional normalization and recognization on the PV-Diagram of reciprocating compressor

The Effect of Impeller Width on the Location of BEP in a Centrifugal Pump

Design and Optimization of Weld Neck Flange for Pressure Vessel

CFD Simulation and Experimental Validation of a Diaphragm Pressure Wave Generator

Stress and deformation of offshore piles under structural and wave loading

Optimization of rotor profiles for energy efficiency by using chamber-based screw model

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

Instruction Manual. Pipe Friction Training Panel

CFD Simulation of the Flow Through Reciprocating Compressor Self-Acting Valves

4.1 Why is the Equilibrium Diameter Important?

A new methodology to evaluate the flying shape of a sail

Hardware Triaxial and Consolidation Testing Systems Pressure Measurement and Control

PG9607 Piston Gauge. Automated primary pressure reference for absolute and gauge pressures to 500 kpa

Bending Vibration Analysis of Pipes and Shafts Arranged in Fluid Filled Tubular Spaces Using FEM

Flow and Mixing in the Liquid between Bubbles

NUMERICAL INVESTIGATION OF PRESSURE DROP IN HYDRAULIC SPOOL VALVE

DIAGNOSTICS OF IMPULSE LINE BLOCKAGE WITH A MULTI-SENSING DIFFERENTIAL PRESSURE TRANSMITTER AT THE AIR LINE

Australian Journal of Basic and Applied Sciences. Pressure Distribution of Fluid Flow through Triangular and Square Cylinders

Effects of Changes of Spokes in the Operation of a Rimmed Flywheel

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

Research on ESC Hydraulic Control Unit Property and Pressure Estimation

Prognosis of Rudder Cavitation Risk in Ship Operation

CORESTA RECOMMENDED METHOD N 6

Gas Spring Losses in Linear Clearance Seal Compressors

Irrigation &Hydraulics Department lb / ft to kg/lit.

Experimental Determination of Temperature and Pressure Profile of Oil Film of Elliptical Journal Bearing

Design and Safety Document for the Vacuum Windows of the NPDGamma Liquid Hydrogen Target at SNS

Badan Jadrowych Nuclear Research Institute. Report INR No. 739/XIX/D CERN LIBRARIES, GENEVA CM-P Differential Recombination Chamber

Transcription:

Proceedings, XVII IMEKO World Congress, June 22 27, 2, Dubrovnik, Croatia Proceedings, XVII IMEKO World Congress, June 22 27, 2, Dubrovnik, Croatia TC TC6 XVII IMEKO World Congress Metrology in the rd Millennium June 22 27, 2, Dubrovnik, Croatia DESIGN AND CHARACTERISATION OF A DOUBE-PISTON PRESSURE BAANCE IN HIGH PRESSURE G. Buonanno, M. Dell'Isola, A. Frattolillo Di.M.S.A.T., University of Cassino, Cassino, Italy Abstract The paper describes the design and the analysis of a new kind of pressure balance intended to operate up to 5 MPa. The design can be considered as a calculation test to evaluate the possibility to produce a pressure balance whose changes in effective area with pressure (and, consequently, the elastic distortions) are small if compared to other pressure balances operating in the same pressure range and, furthermore, it presents an etended measurement range. The method used for the theoretical characterisation is an improvement of a numerical method using a finite element method. Keywords: Pressure balance, Double-piston. INTRODUCTION The development of innovative high pressure production technologies and the scientific interest in determining the thermophysical properties of materials has increased, in the last years, the attention paid to high pressure metrological traceability. Pressure balances are widely used over a very wide range (from kpa up to GPa and above) for the generation of primary standards of pressure []. Currently conventional pressure balances that operate at very high pressure are based on re-entrant and controlled clearance modes, and also moderately on free-deformation (simple) mode up to 5 MPa. Several studies on innovative pressure balances were carried out in the last years in order to etend the metrological performances to very high pressure [2] or to increase the rangeability of pressure balances []. Recently, the Warsaw University of Technology investigated and proposed a new kind of pressure balance combining the advantages of both simple and re-entrant balances [4]. The effective area typically increases with pressure in simple units while it decreases in re-entrant units. In mied units a self-compensation of these two opposite effects can be observed, with the advantage of etending the operating range without using another pressure control system. A mied unit operating up to GPa was designed and built at Warsaw University and studies based on Zhokhowski s simplified model and Finite Element Analysis to etend the measurement range up to 2.6 GPa were presented in [2, 5-6]. On the other hand, in [] an innovative dual-range pressure balance was designed and made by Budenberg Gauge Co td. This pressure balance is constituted by two coaial pistons of different diameter, the one of small diameter fitting closely the larger. At low pressures the larger piston acts in the usual way whereas if the pressure become higher it comes against a stop and the smaller piston takes over. In any case, as regards pressure balances, it is important that the most important design and operative parameters, such as the pressure distortion coefficient, λ, that allows to estimate the change in the effective area, A e, and the piston fall rate, v, be well understood to keep errors and uncertainties to a minimum. At higher pressures (over 5 MP the change in the effective area due to elastic distortion of the piston and cylinder becomes a significant source of uncertainty []. For eample, if a piston-cylinder unit has a pressure distortion coefficient l equal to.8-6 MPa- and considering uncertainties of A e and A of 5 and ppm respectively, for a pressure of MPa, a λ uncertainty of 4% is obtained and from the uncertainty contribution will be.2 ppm. Consequently in the primary calibration field, in order to obtain the best uncertainty in the pressure measurement, both low l values and related uncertainty less than % have to be obtained [7]. The change in Ae with pressure is described by [8]: Ae( p) = A + f( p) () where A is the effective area at reference conditions and f(p) models the change in area with pressure (generally a f p = λ p is used). Recently, different linear model ( ) theoretical methods to evaluate the pressure distortion coefficient by the analytical [7, 9-] or numerical solution [2, -] of a system of differential equations were developed. In the present work, the authors propose a new kind of pressure balance able to limit the elastic distortions in the clearance gap at high pressures and, in the meantime, to etend the measurement range to lower pressures. The main difficulty in designing the pressure balance was to limit the piston fall rate. Both to design and to theoretically characterise a 5 MPa pressure balance, a FEA method is used, that is an improvement of a numerical method reported in [2]. 2. THE DESIGN OF THE DOUBE-PISTON PRESSURE BAANCE This new kind of pressure balance proposed differs from a conventional piston-cylinder unit because of the eistence

Proceedings, XVII IMEKO World Congress, June 22 27, 2, Dubrovnik, Croatia Proceedings, XVII IMEKO World Congress, June 22 27, 2, Dubrovnik, Croatia TC TC6 of two gaps. In fact, the pressure balance is made up of two concentric pistons (Fig. ). Figure gives a schematic overview of the 5 MPa pressure balance, showing its most important geometric characteristics. The unit can indifferently work in high pressure range with the internal cylinder joined to the eternal one or in low pressure with the internal piston joined to the eternal one constituting only one piston. In any case, the pressure acts, independently from the pressure range adopted, both in the internal and the eternal gap. Thus, the characteristic working mode allows one to etend the measurement range also at lower pressures (typically a pressure balance operates with an acceptable repeatability only for measurement pressure higher than 5% of the full scale). Furthermore, the particular geometry allows to obtain very small change of the effective area versus the measurement pressure and a piston fall rate value not very high despite of the presence of two clearance gaps. Fig.. Schematic view of the 5 MPa pressure balance Both cylinder and piston are designed in tungsten carbide, selected with a Young modulus E, equal to a 54 GPa and a Poisson modulus ν, equal to.2. As working fluid an ethylene (5%) and glycol (5%) miture is adopted, normally named ethylene-glycol. The ethyleneglycol properties (practically dynamic viscosity η and density ρ versus pressure) are evaluated by using the eperimental data reported in [4]: 6 η p, 2 C =. ep 4 p η/(pa s) if p/gpa (2) ( ) ( ) 2 ρ ( p, 2 C) = 85.9 +.7 p-88. p + 6.94 p ρ/(kg m - ) if p/gpa () 2.. Numerical procedure A numerical procedure is proposed to design and characterise the pressure balance. This procedure uses the piston-cylinder dimensions, material and operating fluid to calculate the distortions and pressure gradients in the clearance. The above mentioned parameters are then used to calculate the piston fall rate and the change of the effective area versus the measurement pressure and they have been etremely important for the design of the unit and for the selection of the appropriate clearances of the piston-cylinder unit. In particular, the evaluation of the effective area is based on the following equation obtained from a balance of the forces acting on the piston []: 2 u() Ae =π rp( ) + 2 + r p ( ) (4) 2 π h( ) dp 2 π du + rp( ) d rp( ) p d p + 2 d p d where the radial elastic displacements of the piston u(), the radial gap h() and the fluid pressure distribution p() are determined using the mechanical theory of elastic equilibrium and fluid and dynamic theory of laminar flow. In particular, the elastic distortions of piston and cylinder, knowing the pressure along the clearance, are obtained using the equilibrium field equations and the compatibility and the design-constitutive (taking care of appropriate boundary conditions) relationships. The solution of the equation system can be numerically obtained via the F.E.A. method allowing the radial clearance dimension of the pistoncylinder engagement to be determined using the following equation: h() = h + U( ) u( ) (5) On the other hand, the fluid-dynamic theory of laminar flow allows the distribution of pressure p() along the clearance to be obtained, provided the clearance radial dimension h() is known. Assuming i) monodimensional laminar flow, ii) stationary regime, iii) Newtonian fluid and iv) constant temperature, one can obtain by means of the Navier-Stokes equation: 6m & η(p) p() = p d π r (6) p ρ(p) h() As regards the FEA method, triangular iso-parametric and aial-symmetrical type elements are used. The number of elements (approimately 8 elements for the cylinder and for each piston) and the mesh type are determined considering a mesh optimisation criterion. In particular Zienkiewicz-Zhu criterion is used [5]. Finally, as regards to the convergence and consistence of the numerical solution, the moving average criterion is applied. 2.2. Design optimisation Figure 2 shows the final geometry of the model adopted as result of the optimisation analysis with the corresponding coordinates of the most important points reported in Tab. I. Respect to the simple double-piston unit, the following modifications were adopted: a cross-section reduction is added over the eternal gap to increase the pressure losses and then to diminish the piston fall rate; the internal gap in the lower part of the engagement is increased to avoid interferences. As regards the boundary conditions, it is necessary to consider that the measurement pressure is applied also on sd and qg and that the gap between the second piston and the cylinder is composed of two different engagement with

Proceedings, XVII IMEKO World Congress, June 22 27, 2, Dubrovnik, Croatia Proceedings, XVII IMEKO World Congress, June 22 27, 2, Dubrovnik, Croatia TC TC6 two different pressure distribution (with the same pressure value in the section k-t-v-u). h/ µ m 2.5 5 MPa.5 4 MPa 25 MPa MPa 5 MPa -.5.2.4.6.8 Fig. 2. Geometric model TABE I. Coordinates of the most important points Points r/mm z/mm a b c d s e f g h q k t I M N P U V 8 4.5 4.5 8 4.5 4.5 4.58.52.52 4.52 4.52 4.52 4.58 7 7 28 7 7 28 7. NUMERICA RESUTS The dimensionless internal pressure, p = p( )/p m, and the gap radial variation for the internal engagement of the pressure balance proposed are showed in Fig. as the dimensionless aial coordinate, = / sb, varies (where = corresponds to the point s and = to the point. In particular, the gap profile increases as the pressure increases showing a maimum value of 2. µm for a measurement pressure equal to 5 MPa. As regards the pressure profile, it is a parabolic one with a concavity that increases as the pressure increases (see Fig.. This trend is similar to the ones reported in [, ]. p.8.6.4.2 5 MPa 5 MPa.2.4.6.8 Fig.. Radial gap variation and dimensionless pressure in the internal gap as the aial coordinates varies. In Fig. 4, the dimensionless pressure and eternal gap variation for the pressure balance reported in Fig. 2 are showed as the dimensionless aial coordinate varies (where = corresponds to the point h and = to the point f). As regards the gap profile, the range can be divided in two parts: a first one (.857) where the values are high with a maimum value of 8.2 µm for a measurement pressure of 5 MPa and a second one (.857 ) with a reduced values of the gap. The relevant part of the pressure drop is found in the second part of the engagement (see Fig. 4 confirming the importance of the cross section reduction adopted.

Proceedings, XVII IMEKO World Congress, June 22 27, 2, Dubrovnik, Croatia Proceedings, XVII IMEKO World Congress, June 22 27, 2, Dubrovnik, Croatia TC TC6 h/ µ m 8 7 5 MPa sae.2 6 4 MPa 5 4 25 MPa -.2 sae (eternal gap) sae (internal gap) -.4 2 MPa 5 MPa -.6.2.4.6.8 -.8 2 4 5 p.8 v/(mm/s).25.2.6.5.4..2.5.2.4.6.8 Fig. 4. Radial gap variation and dimensionless pressure in the eternal gap as the aial coordinates varies. Figs and 4 show a good performance of the pressure balance referred to gap and pressure profile but the geometric optimisation allows to obtain small changes of the effective area. In fact, in Fig. 5a the effective area presents a negative trend and the corresponding variations respect to the effective area at reference condition (defined as sae = ( Ae A ) / A) are less than 6 ppm. These values were obtained introducing the cross section reduction and in Fig. 5b the piston fall rate is reported as the measurement pressure varies. The change in the effective area are etremely small respect to the ones of other pressure balances that operate at high pressure. In Fig 6, a comparison between the change in the effective area and the piston fall rate of the pressure balance designed and the ones of two comple units [, 6] in high pressure range is reported. 2 4 5 Fig. 5. Effective area and piston fall rate versus the measurement pressure. As regards the use of the present pressure balance at lower pressure, the pressure distortion coefficient considering the eternal gap is equal to.94-6 MPa -, value that is compatible with the ones usually referred to similar pressure balances [, 7,, 6]. 4. CONCUSIONS The present study designs and analyses a new kind of pressure balance intended to operate up to 5 MPa, able to limit the elastic distortions in the clearance gap at high pressures and, in the meantime, to etend the measurement range to lower pressures. The unit, made up of two concentric pistons, can indifferently work in high pressure range with the internal cylinder joined to the eternal one or in low pressure with the internal piston joined to the eternal one constituting only one piston. From the numerical results, the change in the effective area are etremely small respect to the ones of other pressure balances that operate at high pressure. The main

Proceedings, XVII IMEKO World Congress, June 22 27, 2, Dubrovnik, Croatia Proceedings, XVII IMEKO World Congress, June 22 27, 2, Dubrovnik, Croatia TC TC6 difficulty in designing the pressure balance was to limit the piston fall rate. sae/(%).5.4..2..4 v/(mm/s) Present pressure balance -. 2 4 5...25.2.5..5 2 4 5 6 Present pressure balance Fig. 6. Change of the effective area and piston fall rate versus the measurement pressure 6 [5] Wisniewski R. and G. Molinar, Pressure standards and sensors up to GPa, Conference Proceedings of the XXXVI EHPRG Conference, Catania, Italy, 7- September 998, Physica B, 265, 999, 246-25 [6] Wisniewski R. and G. Molinar, High Pressure Tester up to 2,5 GPa with very accurate pressure to force transducer suitable for optic and electric measurement methods, Presented at Symposium "New Tendencies in Measurements of High Pressures" Jadwisin, Poland, -5 June996, Editor Warsaw University of Technology, Prof. R. Wisniewski and Dr. A. Magiera, 997, 64-68 [7] Molinar G.F., Maghenzani R., Cresto P.C. and. Bianchi, 992, Elastic distortions in piston-cylinder units at pressures up to.5 GPa, Metrologia, 29, 425-44. [8] Fitzgerald M.P., Sutton C.M. and D.G. Jack, 999, Design of a pressure balance with a small and calculable change of area with pressure, Metrologia, 6, 57-57 [9] McIlraith A.H. and M.P. Fitgerald, 992, Analysis of controlled clearance seals, Metrologia, 29, 285-29 [] Buonanno G., Dell'Isola M. and A. Frattolillo, Simplified analytical methods to evaluate the pressure distortion coefficient of clearance controlled pressure balances, submitted to High Temperatures - High Pressures [] Buonanno G. and M. Dell'Isola, 2, Design and metrological characterisation of different pressure balances using finite element method, High Temperatures - High Pressures, 2, 89-98 [2] Buonanno G., Dell'Isola M., Iagulli G., and G.F. Molinar, 999, A finite element method to evaluate the pressure distortion coefficient in pressure balances, High Temperatures - High Pressures,, n.2, -4 [] Buonanno G., Dell'Isola M. and R. Maghenzani, 999, Finite Element Analysis of Pressure Distortion Coefficient and Piston Fall Rate in a Simple Pressure Balance, Metrologia, 6, n. 6, 579-584 [4] Wisniewski personal communication, 998 [5] Zienkiewiecz O.C. and R.. Taylor, 2, The finite element method, 5th ed. Butterworth-Heinemann, Oford [6] Molinar G., Bergoglio M., Buonanno G., Dell Isola M., Giovinco G., Parametric analysis of the PTB (7594 DH) piston cylinder unit operating up to GPa, Euromet Project #46, Internal report REFERENCES [] Pavese F., Molinar G.F., 992, in Modern gas-based temperature and pressure measurements, Ed. Timmerhaus K.D., Clark Alan F., Rizzuto C., New York: Plenum Publishing Corporation, 27-6 [2] Buonanno G., Dell'Isola M., Maghenzani R., Molinar G.F., Urbanski M., Wisniewski R., 999, Elastic Distortions of a Mied (Simple & Re-entrant) Piston-Cylinder Unit for Pressure Measurements up to 2,6 GPa, Metrologia, 6, n. 6, 585-59 [] Dadson R S, ewis S, Peggs G N, 982, The pressure balance - Theory and practice, National Physical aboratory, ondon: Her Majesty's Stationery Office [4] Wisniewski R., Urbanski M. and A. Golkowska, The effective area of a pressure balance with a mied principle of operation, High Temperatures-High Pressures, Vol. 4, 982, -4 Authors: Prof. Giorgio Buonanno, (Di.M.S.A.T., School of Engineering), via Di Biasio 4 4 Cassino (FR) Italy, ph. +9 () 776 299669, fa +9 () 776 2999, e-mail: buonanno@unicas.it Prof. Marco Dell Isola, (Di.M.S.A.T., School of Engineering), via Di Biasio 4 4 Cassino (FR) Italy, ph. +9 () 776 29967, fa +9 () 776 2999, e-mail: dellisola@unicas.it Eng. Andrea Frattolillo, (Di.M.S.A.T., School of Engineering), via Di Biasio 4 4 Cassino (FR) Italy, ph. +9 () 776 2999, fa +9 () 776 2999, e-mail: frattolillo@unicas.it