Streamline tracing technique based design of elliptical-to-rectangular transitioning hypersonic inlet

M. Rizal Rosli, Masahiro Takahashi, Tetsuya Satou, Takayuki Kojima, Hideyuki Taguchi, Yusuke Maru

Research output: Contribution to conferencePaper

1 Citation (Scopus)

Abstract

Design of an elliptical-to-rectangular transitioning hypersonic inlet for design Mach number of 5.0 is reviewed. The design approach that has been applied here is based on the streamline tracing technique in a known flowfield, where three-dimensional axisymmetric Busemann inlet is utilized as the flowfield to be modified. The choice of elliptical crosssectional capture and the desirable rectangular throat profile gives advantages in resolving simultaneously two major problems in the former flowfield without assistance of any other additional arrangements. The newly modified inlet provides reduction of approximately 80% in the contraction ratio and of 16.3% in the length of the compression surface.

Original languageEnglish
DOIs
Publication statusPublished - 2013 Jan 1
Event31st AIAA Applied Aerodynamics Conference - San Diego, CA, United States
Duration: 2013 Jun 242013 Jun 27

Conference

Conference31st AIAA Applied Aerodynamics Conference
CountryUnited States
CitySan Diego, CA
Period13/6/2413/6/27

ASJC Scopus subject areas

  • Aerospace Engineering
  • Mechanical Engineering

Fingerprint Dive into the research topics of 'Streamline tracing technique based design of elliptical-to-rectangular transitioning hypersonic inlet'. Together they form a unique fingerprint.

  • Cite this

    Rizal Rosli, M., Takahashi, M., Satou, T., Kojima, T., Taguchi, H., & Maru, Y. (2013). Streamline tracing technique based design of elliptical-to-rectangular transitioning hypersonic inlet. Paper presented at 31st AIAA Applied Aerodynamics Conference, San Diego, CA, United States. https://doi.org/10.2514/6.2013-2665