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Experimental Study of Chin Intakes for Airbreathing Missiles with High Agility

  • Published:2008-03 Issue:2 Volume:24 Page:236-244
  • ISSN:0748-4658
  • Container-title:Journal of Propulsion and Power
  • language:en
  • Short-container-title:Journal of Propulsion and Power

Author:

Herrmann Dirk1,Triesch Klaus1,Gülhan Ali1

Affiliation:

1. Institute of Aerodynamics and Flow Technology German Aerospace Center, 51147 Cologne, Germany

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Reference28 articles.

1. AIAA Education Series;Seddon J.,1985

2. AIAA Education Series;Seddon J.,1993

3. Experimental Study on Restart Control of a Supersonic Air-Breathing Engine

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1. Aerodynamic Instabilities in High-Speed Air Intakes and Their Role in Propulsion System Integration;Aerospace;2024-01-12

2. Computation of viscous flow characteristics of a supersonic intake using eddy-viscosity turbulence models;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2022-07-06

3. Effects of boundary-layer bleed parameters on supersonic intake buzz;Aerospace Science and Technology;2022-01

4. Experimental investigation into the effects of Mach number and boundary-layer bleed on flow stability of a supersonic air intake;SCI IRAN;2020

5. Boundary layer suction for high-speed air intakes: A review;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2018-08-13
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