'Pressure ratio' diaporamas de présentation

Plasticity in sensory systems

1.12k views • 91 slides

Optimal Design of Gas Turbine Power Station

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FIRES EXPLOSIONS

FIRES EXPLOSIONS. AND. FUNDAMENTALS and DESIGN CONSIDERATIONS. Harry J. Toups LSU Department of Chemical Engineering with significant material from SACHE 2003 Workshop presentation by Ray French (ExxonMobil). Fuels: Liquids gasoline, acetone, ether, pentane Solids

730 views • 61 slides

Sky By OceanAire

Sky By OceanAire. Poorvi Kalaria Roman Maire Andy Grimes Motohide Ho Tara Palmer Greg Freeman Vicki Huff Nick Gurtowski Jack Yang Sanjeev Ramaiah. System Definition Review. Mission Objectives Design Requirements Aircraft Concept Selection

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Joint Heavy Lift(JHL) -JSF Lift Fan Derivative

Joint Heavy Lift(JHL) -JSF Lift Fan Derivative. Kevin Ferguson Juan Gutierrez Phil Lines. Ryan Aaron Chris Bradshaw Jesus Claudio Romen Cross. Scope of Presentation. Mission Overview Design Characteristics Initial Engine Design Final Engine and Fan Design Driveshaft/Gearbox Design

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22.033 Final Design Presentation

22.033 Final Design Presentation. Vasek Dostal Knut Gezelius Jack Horng John Koser Joe Palaia Eugene Shwageraus And Pete Yarsky With the Help of Kalina Galabova Nilchiani Roshanak Dr. Kadak. Outline. Mission plan Space power system Surface power system Conclusions Future Work.

558 views • 42 slides

Mathematics-in-Action Engine Design Workshop

Mathematics-in-Action Engine Design Workshop. Ian Halliwell Senior Research Scientist Avetec Inc, Springfield, Ohio July 21, 2008. Contents. 1. The Role of Mathematics in the Design of Gas Turbine Engines Mathematics, Science & Engineering The Preliminary Design Process Detailed Design

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Lecture 6

Lecture 6. Turbojet Optimization Cycle selection (mission dependency) Indication of thrust Convergent-divergent nozzles Turbofan Cycle optimization Mixing Increasing thrust (afterburning) Turboprops Problem 3.2. Optimization of the turbojet.

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COGAS Propulsion for LNG Ships

COGAS Propulsion for LNG Ships. September 11, 2007 Edwin G. Wiggins Rosenblatt Professor of Marine Engineering. LNG Ship Propulsion. Steam turbine without reheat until very recently Steam turbine with reheat has been proposed. LNG Ship Propulsion. Medium speed diesel

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Lecture 8

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GAS TURBINE POWER PLANTS

GAS TURBINE POWER PLANTS. Gas turbines tend to be lighter and more compact than the vapour power plants. Gas turbines are used for stationary power generation.

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Chapter Seven

Chapter Seven. Compressible Fluid. Introduction. When a fluid moves at speeds comparable to its speed of sound, density changes become

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Welcome to 2040

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Chapter 21 Theoretical Rates in Closed-Channel Flow

Chapter 21 Theoretical Rates in Closed-Channel Flow. Many a time did I stand such a pipe and exert myself to invent how to force these pipes so reveal the secret of their hidden action. Clemens Herschel (1898). 21.1 General Remarks

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AME 436 Energy and Propulsion

AME 436 Energy and Propulsion. Lecture 10 Propulsion 1: Thrust and aircraft range. Outline. Why gas turbines? Computation of thrust Propulsive, thermal and overall efficiency Breguet range equation. GE CT7-8 turboshaft (used in helicopters)

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OUTLINE Concept Development of a He - beam Development of a HeH + beam

R & D Status of Beam Neutralization System M. Sasao, K. Shinto, M. Okamoto, S. Kitajima, N. Tanaka, M. Nishiura, O. Kaneko, H. Sakakida, and M. Wada Tohoku Univ. NIFS, AIST,and Doshisha Univ. OUTLINE Concept Development of a He - beam Development of a HeH + beam

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GeV Gamma-ray Observations of Galaxy Clusters with the Fermi LAT

GeV Gamma-ray Observations of Galaxy Clusters with the Fermi LAT . Keith Bechtol representing the Fermi LAT Collaboration July 14, 2009. Non-thermal view of galaxy clusters. Galaxy clusters cannot be described by mass alone! Non-thermal window Precision cosmology

324 views • 15 slides

Elements of ICAO CAEP Approach

International Civil Aviation Organization Colloquium on Environmental Aspects of Aviation Aircraft Emissions - The Way Forward Willard Dodds, Chairman ICCAIA Noise and Emissions Committee Montreal, 9-11 April 2001. Elements of ICAO CAEP Approach. Terms of Reference

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Reciprocating Compressor

720 views • 8 slides