Optimization Design of the Flush Air Data System

Qing Feng Zhang

doi:10.4028/www.scientific.net/AMM.533.312

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 533Optimization Design of the Flush Air Data System

Optimization Design of the Flush Air Data System

Abstract:

A new configuration of multi sensor flush air data system was proposed and the detecting principles of the flush air data system was discussed. A large number of redundant information pick up from multi sensors embedded in aircraft data system put forward the requirements of information optimization. Characteristic value of air data defined in this chapter meet the active control system of aircraft redundancy requirements of total pressure, static pressure, angle of attack and sideslip angle of atmospheric data, was the foundation of the multi sensor information fusion system.

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Periodical:

Applied Mechanics and Materials (Volume 533)

Pages:

312-315

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.533.312

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Online since:

February 2014

Authors:

Qing Feng Zhang

Keywords:

Aerospace Plane, Flush Air Data System, Hypersonic Speed, Optimization

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References

[1] Larson, T J, Whitmore S A, Ehernberger L J, Qualitative evaluation of a flush air data system at transonic speeds and high angles of attack. NASA-TP-2716, (1987).

Google Scholar

[2] Anderson J D Jr. Hypersonic and high temperature gas dynamics. New York: Grawhill book Company, (1998).

Google Scholar

[3] Murray A l, Lewis C H, Hypersonic three dimensional viscous shock-layer flows over blunt bodies, AIAA, Journal, 1978, 16(12): 1279-1286.

DOI: 10.2514/3.61044

Google Scholar

[4] Helliwell W S, Dickinson R P, Lubard S C, Viscous flow over arbitrary geometries at high angle of attack, AIAA-80-0064.

DOI: 10.2514/3.50940

Google Scholar

[5] Shanks S P, Sprinivasan G R, Nicolet W E, AFWAL Parabolized navier-stokes code: formalization and user's manual, 1982, AFWAL-TR-3234.

Google Scholar

[6] Gnoffo P A, an Upwind-biased point-implicit relaxation algorithm for viscous, Compressible Perfect Gas Flows, NASA, feb 1990, TP-2953.

DOI: 10.2514/6.1989-1972

Google Scholar

[7] Aerosoft, GASP version 3, the general aerodynamic simulation program, computational flow analysis software for the scientist and engineer, User's Manual, Aerosoft Inc, Blacksburg, 1996 May, VA.

Google Scholar