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A proposed design method for supersonic inlet to improve performance parameters

  • Published:2019-08 Issue: Volume:91 Page:583-592
  • ISSN:1270-9638
  • Container-title:Aerospace Science and Technology
  • language:en
  • Short-container-title:Aerospace Science and Technology

Author:

Farahani M.ORCID,Mahdavi M.M.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference26 articles.

1. Study of buzz phenomenon using visualization of external shock structure;Farahani;Proc. Inst. Mech. Eng. G, J. Aerosp. Eng.,2018

2. Novel method for supersonic inlet buzz measurement in wind tunnel;Daliri;J. Propuls. Power,2017

3. Effects of bleed position on the stability of a supersonic inlet;Soltani;J. Propuls. Power,2016

4. Buzz cycle description in an axisymmetric mixed-compression air intake;Soltani;AIAA J.,2015

5. Effects of angle of attack on inlet buzz;Soltani;J. Propuls. Power,2012

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1. Comparative performance analysis of supersonic inlets at various Mach number;AIP Conference Proceedings;2024

2. Fast multi-objective optimization design of gas turbine L-inlet duct;Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy;2023-11-14

3. Experimental and numerical study on aerodynamic stability of compressor L-inlet duct;Aerospace Science and Technology;2023-08

4. Mixed-Compression Supersonic Intake and Engine–Airframe Integration;Journal of Spacecraft and Rockets;2023-07

5. Fully Parabolic Prediction of the Hypersonic Near-Field About Slender Axisymmetric Bodies;AIAA SCITECH 2023 Forum;2023-01-19
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