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Performance Analysis of Supersonic Intake Systems in Aircraft

This document presents an in-depth performance analysis of various types of supersonic intake systems, including axi-symmetric inlets and the Concorde intake systems. It covers key concepts such as weak and strong oblique shocks, adiabatic flow analyses, and temperature-entropy diagrams. The report also examines the overall performance of inlets and discusses options for improving supersonic intake efficiency, taking into account gas dynamics principles and the governing equations that describe the flow behavior within these systems.

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Performance Analysis of Supersonic Intake Systems in Aircraft

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    1. Performance Analysis of Intake Systems P M V Subbarao Professor Mechanical Engineering Department I I T Delhi

    2. Supersonic Engines

    4. Supersoinc Intakes

    5. Axi-Symmetric Inlets for Supersonic Speeds

    6. Weak And Strong Oblique Shock

    7. Concorde Intake Systems

    9. Performance of An Adiabatic Oblique Shock

    11. Overall Performance of An Inlet

    13. Options for Supersonic Intakes

    14. Temperature Entropy Diagram

    15. Temperature Entropy Diagram

    16. Temperature Entropy Diagram

    17. Temperature Entropy Diagram

    18. Temperature Entropy Diagram

    19. Temperature Entropy Diagram

    20. Selection of A System of Irriversibilities

    21. Gas Dynamics of Intake Systems : Frictional Flow with Heat Transfer

    22. Governing Equations

    26. System of Equaions

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