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ESDU International PLC
Books by Publisher: ESDU International PLC
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Dwell-rise-fall-dwell and Dwell-fall-rise-dwell Cam Laws: Segments Having Equal Rise and Fall Periods, 06002: Sections 1 to 8 (Mechanisms)
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Aircraft Performance Program: Introduction to the Computer Programs for Aircraft Performance Evaluation. 00031: Pt. 1
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Falling Film Evaporation in Vertical Tubes. 98010
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Elastic Stresses and Deflections Under Uniform Pressure of Flat Rectangular Sandwich Panels; All Edges Clamped (Isotropic Face Plates and Orthotropic Cores of Zero Flexural Stiffness). 77003
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Performance of Conical Diffusers in Incompressible Flow. 73024
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Vapour Pressures and Critical Points of Liquids: Alkadienes and Alkynes. 86001: Pt. 2C
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Wing Pitching Moment at Zero Lift at Subcritical Mach Numbers. 87001
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Guide to the Use of ESDU Data Items on Cam Design. 01002
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A Framework Relating the Drag-rise Characteristics of a Finite Wing/body Combination to the Those of Its Basic Aerofoil. 78009
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Normal Melting Points,Boiling Points and Critical Points of Monobasic Alkanoic Acids. 72006
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Flexibility Of,and Load Distribution In,Multi-bolt Lap Joints Subject to In-plane Axial Loads. 98012
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Information on the Use of Data Items on Hot Structures. 89021
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The Lift Achievable by Aerofoils Having a Particular Form of Supercritical Upper-surface Pressure Distribution That Yields Only Small Wave Drag. 78010
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Approximate Estimation of Drag of Windmilling Propellers (Performance)
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Validated Engineering Data Index 1997-1998
No stated author
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Information for the Use of Data Items on High-lift Devices. 97002
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Example of Risk Analysis Applied to Aircraft Landing Distance (Performance of Aircraft)
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Estimation of Far-field Sound Pressure Levels Due to Buzz-saw Noise of a Supersonic Fan or Compressor. 75020
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Example of Risk Analysis Applied to En-Route Flight Path for Large Jet Transport Aircraft (Performance of Aircraft)
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OSMEC. Computer-aided Linkage Design: Installation. 97023
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OSMEC. Computer-aided Linkage Design: User Manual. 97026
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Wing Lift Coefficient Increment at Zero Angle of Attack Due to Deployment of Plain Trailing-edge Flaps at Low Speeds. 97011
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Lift Curve of Wings with High-lift Devices Deployed at Low Speeds. 96003
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VGK Method for Two-dimensional Aerofoil Sections: Principles and Results. 96028: Pt. 1
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Estimation of Noise Shielding by Barriers 79011
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Treatment of Risk within Commercial Air Transport (Performance of Aircraft)
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Wing Lift Coefficient Increment at Zero Angle of Attack Due to Deployment of Trailing-edge Split Flaps at Low Speeds. 97009
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Introduction and Guide to ESDU Data on Acoustic Fatigue. 74037
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Pitot and Static Errors Due to Non-steady Flight. 85011
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Thermophysical Properties of Toluene: The Ideal Gas and the Saturated Liquid and Vapour. 88009: Pt. I
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Effect of Gap on the Slope of Lift Curve and Slope of Lift Increment Curve Due to Control Surface Deflection: Amendment A (Aerodynamics)
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Propeller Slipstream Modelling for Incidence and Sideslip, 06013: Pt. 8b (Aerodynamics)
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