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Aerodynamics / Shock waves / Unstart / Wave / Moving shock / Shock / Mach number / Fluid dynamics / Dynamics / Fluid mechanics


JOURNAL OF AIRCRAFT Vol. 41, No. 4, July–August 2004 Dynamics and Control of Shock Motion in a Near-Isentropic Inlet Douglas G. MacMartin∗ California Institute of Technology, Pasadena, California 91125
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Document Date: 2006-05-30 22:19:00

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City

Danvers / Opalski / Pasadena / New York / /

Company

Dynamical Systems / Clearance Center Inc. / VI.C. / Aeronautics and Astronautics Inc. / /

Currency

USD / /

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Facility

American Institute / Massachusetts Institute of Technology / California Institute of Technology / Isentropic Inlet Douglas G. MacMartin∗ California Institute of Technology / /

IndustryTerm

control algorithm / smooth control law / control law µa / discontinuous time-delayed control law / control law µb / nominal solution / series feedback network / smooth control law µa / feedback control law / control law / energy / /

Organization

California Institute of Technology / Copyright Clearance Center / American Institute / US Federal Reserve / B. Authority / Massachusetts Institute of Technology / U.S. Securities and Exchange Commission / Department of Control and Dynamical Systems / /

Person

Ali Merchant / Timothy Colonius / James Paduano / Euler / /

Position

smooth controller / simple controller / simple time-delay controller / forward / /

ProvinceOrState

California / A. B. / Massachusetts / /

Technology

control algorithm / simulation / /

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