Numerical simulation of HSCT inlet operability with angle of attack

Ge Cheng Zha; Doyle Knight; Donald Smith; Martin Haas

Numerical simulation of HSCT inlet operability with angle of attack

Ge Cheng Zha, Doyle Knight, Donald Smith, Martin Haas

School of Engineering, Mechanical & Aerospace Engineering

Rutgers, The State University

Research output: Contribution to conference › Paper › peer-review

1 Scopus citations

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 language	American English
State	Published - 1997
Event	33rd Joint Propulsion Conference and Exhibit, 1997 - Seattle, United States Duration: Jul 6 1997 → Jul 9 1997

Other

Other	33rd Joint Propulsion Conference and Exhibit, 1997
Country/Territory	United States
City	Seattle
Period	7/6/97 → 7/9/97

ASJC Scopus subject areas

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

Cite this

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title = "Numerical simulation of HSCT inlet operability with angle of attack",

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.",

author = "Zha, {Ge Cheng} and Doyle Knight and Donald Smith and Martin Haas",

note = "Publisher Copyright: {\textcopyright} 1997 by Ge-Cheng Zha, Doyle D. Knight, Donald Smith and Martin Haas. Published by the American Institute of Aeronautics and Astronautics, Inc.; 33rd Joint Propulsion Conference and Exhibit, 1997 ; Conference date: 06-07-1997 Through 09-07-1997",

year = "1997",

language = "American English",

}

TY - CONF

T1 - Numerical simulation of HSCT inlet operability with angle of attack

AU - Zha, Ge Cheng

AU - Knight, Doyle

AU - Smith, Donald

AU - Haas, Martin

PY - 1997

Y1 - 1997

N2 - 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.

AB - 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.

UR - http://www.scopus.com/inward/record.url?scp=84962873373&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=84962873373&partnerID=8YFLogxK

M3 - Paper

T2 - 33rd Joint Propulsion Conference and Exhibit, 1997

Y2 - 6 July 1997 through 9 July 1997

ER -

Numerical simulation of HSCT inlet operability with angle of attack

Abstract

Other

ASJC Scopus subject areas

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