Numerical simulation of HSCT inlet operability with angle of attack

GeCheng Zha, Doyle Knight, Donald Smith, Martin Haas

Research output: Chapter in Book/Report/Conference proceedingConference contribution

1 Citation (Scopus)

Abstract

A High Speed Civil Transport (HSCT) inlet at Mach 2 and angle of attack is simulated by using a 3D Navier-Stokes solver with the Baldwin- Lomax algebraic turbulence model. An extrapolation uniform mass bleed boundary condition for the slot bleed is successfully employed. For zero angle of attack and critical operation, the pressure distribution agrees well with the experiment. The location and intensity of the terminal shock, total pressure recovery are accurately computed. The angle of attack to cause the inlet unstart is accurately predicted. The mesh refinement results are presented.

Original languageEnglish (US)
Title of host publication33rd Joint Propulsion Conference and Exhibit
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9780000000002
StatePublished - 1997
Externally publishedYes
Event33rd Joint Propulsion Conference and Exhibit, 1997 - Seattle, United States
Duration: Jul 6 1997Jul 9 1997

Other

Other33rd Joint Propulsion Conference and Exhibit, 1997
CountryUnited States
CitySeattle
Period7/6/977/9/97

Fingerprint

Angle of attack
Computer simulation
Turbulence models
Extrapolation
Pressure distribution
Mach number
Boundary conditions
Recovery
Experiments

ASJC Scopus subject areas

  • Energy Engineering and Power Technology
  • Electrical and Electronic Engineering
  • Mechanical Engineering
  • Control and Systems Engineering
  • Aerospace Engineering

Cite this

Zha, G., Knight, D., Smith, D., & Haas, M. (1997). Numerical simulation of HSCT inlet operability with angle of attack. In 33rd Joint Propulsion Conference and Exhibit American Institute of Aeronautics and Astronautics Inc, AIAA.

Numerical simulation of HSCT inlet operability with angle of attack. / Zha, GeCheng; Knight, Doyle; Smith, Donald; Haas, Martin.

33rd Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics Inc, AIAA, 1997.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Zha, G, Knight, D, Smith, D & Haas, M 1997, Numerical simulation of HSCT inlet operability with angle of attack. in 33rd Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics Inc, AIAA, 33rd Joint Propulsion Conference and Exhibit, 1997, Seattle, United States, 7/6/97.
Zha G, Knight D, Smith D, Haas M. Numerical simulation of HSCT inlet operability with angle of attack. In 33rd Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics Inc, AIAA. 1997
Zha, GeCheng ; Knight, Doyle ; Smith, Donald ; Haas, Martin. / Numerical simulation of HSCT inlet operability with angle of attack. 33rd Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics Inc, AIAA, 1997.
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