Shock Waves (2009) 19:453–468 DOI 10.1007/s00193-009-0220-z ORIGINAL ARTICLE Some physical aspects of shock wave/boundary layer interactions Jean Délery · Jean-Paul Dussauge Received: 9 February 2009 / Accepted: 29 June 2009 / Published online: 26 July 2009 © Springer-Verlag 2009 Abstract When the flow past a vehicle flying at high velocity becomes supersonic‚ shock waves form‚ caused either by a change in the slope of a surface‚ a downstream obstacle or a back pressure constraining the
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Jr.”Fundamentals of Aerodynamics”‚ McGraw-Hill‚ 2001. 2. E.L .Houghton and P.W. Carpenter “Aerodynamics for Engineering Students” Fifth Edition‚ Butterworth-Heinemann publications‚ 2003. 3. B.R Munson‚ P.F Young‚ T.H Okiishi‚ ”Fundamentals of Fluid Dynamics” John Wiley & Sons‚ 2002. 4. Barlow‚ J.B.‚ Rae Jr.‚ W.H.‚ Pope‚ A.‚ Low-Speed Wind Tunnel Testing Wiley & Sons‚ Inc.‚ New York‚ 1999. pp 147-150. 5. Robert C. Platt‚”Turbulence Factors of NACA Wind Tunnels As Determined Sphere Tests”1937. 6. Dryden
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3rd International Conference on Trends in Mechanical and Industrial Engineering (ICTMIE ’2013) January 8-9‚ 2013 Kuala Lumpur (Malaysia) Conceptual Design of Short Takeoff Supersonic Aircraft with Cold Flow Nozzles Vignesh. M 1‚ Sathish. K1‚ Adrin Issai Arasu. L1‚ Dharun Lingam. K1‚ and Sanal Kumar. V.R 2 consumption and poor range) in turn making it unprofitable for manufacturers to produce these kinds of aircraft. It can cover a distance from India to USA in 2 ½ hours. Propulsion systems that
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Figure 2 Ideal Power versus Head Pressure (H) · Sample Calculations · Raw Data Discussion of Experiment A centrifugal pump contains an impeller or set of vanes encased in housing. Energy is added to the fluid in the form of velocity and pressure as a result of the impeller turning. An engineer must determine the range of flow rates required when using a centrifugal pump. The centrifugal pump chosen for an application must have a head versus flow rate
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Group Case 1 Group 5 2/27/13 Microsoft Dynamics Customer Solution Case Study: Nonprofit Empowers Team‚ Markets More Effectively with Association Management Solution Background of the Organization National Middle School Association is a nonprofit organization. They have 25 employees that provide professional development‚ journals‚ books‚ research‚ and information to middle school teachers in the United States. NMSA generates about $6.5 million a year in revenue through membership fees
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used as a control valve. The conditions such as pressure of the pipeline system have to be suitable for the valves used. The hazards and safety practice involved in this experiment are very vital in industrial use especially when there are explosive fluids involved. Experimental Setup: Manometer Manometer Tapered Side Tapered Side Orifice Plate Orifice Plate Globe Valve Globe Valve Gate Valve Gate Valve Pump/Blower Pump/Blower Legends Flow of air Flow of air Hazards and Safety
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CHILINGARIAN (Editors) OIL SHALE 6 D.W. PEACEMAN FUNDAMENTALS OF NUMERICAL RESERVOIR SIMULATION 7 G.V. CHILINGARIAN and T.F. YEN (Editors) BITUMENS‚ ASPHALTS AND TAR SANDS 8 L.P. DAKE FUNDAMENTALS OF RESERVOIR ENGINEERING 9 K. MAGARA COMPACTION AND FLUID MIGRATION 10 M.T. SILVIA and E.A. ROBINSON DECONVOLUTION OF GEOPHYSICAL TIME SERIES IN THE EXPLORATION FOR OIL AND NATURAL GAS Developments in Petroleum Science‚ 8 fundamentals of reservoir engineering LP. DAKE Senior Lecturer in Reservoir
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TOC Previous Next Table of Contents Chapter 1 : Pore Pressure Chapter 2 : Formation Integrity Tests Chapter 3 : Kick Tolerance Chapter 4 : Casing Functions & Types Chapter 5 : Casing Design Principles Chapter 6 : Cementing Chapter 7 : Drilling Fluids Chapter 8 : Practical Rig Hydraulics Chapter 9 : Drill Bits Chapter 10 : Drillstring Design Chapter 11 : Directional Drilling Chapter 12 : Hole Problems Chapter 13 : Horizontal & Multilateral Wells Chapter 14 : Rig Components Chapter 15 : Well Costing
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Queen Mary‚ University of London School of Engineering and Materials Science Den233 Low Speed Aerodynamics Pressure Distribution and Lift on a Piercy Aerofoil Abstract In this experiment in a low speed flow the static pressure around an aerofoil will be observed and discussed. The lift on the aerofoil will also be calculated and compared with the theoretical value. The aerofoil being used in this particular experiment is
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Summary The topic investigated in this report is heat transfer in a concentric tube heat exchanger. A heat exchanger is a device used to transfer heat from a hot fluid to a colder fluid. Heat exchangers are widely used in the petroleum industry for various reasons. Some of the most important reasons are theta heat exchangers increase the process efficiency‚ conserve energy‚ reduce maintenance and provide employee safety among many other reasons. The main objectives of the lab study were to determine
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