SAE AIR1168/V1 SAE Aerospace Applied Thermodynamics Manual
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Product Code:SAE AIR1168/V1
Title:SAE Aerospace Applied Thermodynamics Manual
Issuing Committee:
Scope:The SAE Aerospace Applied Thermodynamics Manual has long been the industry reference on aerodynamics, heat transfer, fluid dynamics, and materials properties. Now, over 20 years since the last edition was published, the third edition is available. Reflecting over 1,000 corrections from the previous version, this valuable manual is comprised of 10 individual paperbound books that are shrinkwrapped as a set. Economically priced, the manual includes books devoted to these topics: Thermodynamics of Incompressible and Compressible Fluid Flow; Aerothermodynamic Systems Engineering and Design; Ice, Rain, Fog, and Frost Protection; Aerothermodynamic Test Instrumentation and Measurement; Characteristics of Equipment Components, Equipment Cooling System Design, and Temperature Control System Design; Aerospace Pressurization System Design; Aircraft Fuel Weight Penalty Due to Air Conditioning; Thermophysical Properties of the Natural Environment, Gases, Liquids, and Solids; Thermophysical Characteristics of Working Fluids and Heat Transfer Fluids; and Spacecraft Life Support Systems.
Title:SAE Aerospace Applied Thermodynamics Manual
Issuing Committee:
Scope:The SAE Aerospace Applied Thermodynamics Manual has long been the industry reference on aerodynamics, heat transfer, fluid dynamics, and materials properties. Now, over 20 years since the last edition was published, the third edition is available. Reflecting over 1,000 corrections from the previous version, this valuable manual is comprised of 10 individual paperbound books that are shrinkwrapped as a set. Economically priced, the manual includes books devoted to these topics: Thermodynamics of Incompressible and Compressible Fluid Flow; Aerothermodynamic Systems Engineering and Design; Ice, Rain, Fog, and Frost Protection; Aerothermodynamic Test Instrumentation and Measurement; Characteristics of Equipment Components, Equipment Cooling System Design, and Temperature Control System Design; Aerospace Pressurization System Design; Aircraft Fuel Weight Penalty Due to Air Conditioning; Thermophysical Properties of the Natural Environment, Gases, Liquids, and Solids; Thermophysical Characteristics of Working Fluids and Heat Transfer Fluids; and Spacecraft Life Support Systems.
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