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Mathematical description of aircraft longitudinal aerodynamic characteristics at high angles of attack accounting for dynamic effects of separated flow
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Goman, M.G.1
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State-space representation of aerodynamic characteristics of an aircraft at high angles of attack
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Goman, M.G.1
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Validation of methodology for estimating aircraft unsteady aerodynamic parameters from dynamic wind tunnel tests
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AIAA Washington, DC
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Murphy, Patrick C. and Klein, Vladislav, "Validation of Methodology for Estimating Aircraft Unsteady Aerodynamic Parameters From Dynamic Wind Tunnel Tests, " AIAA Atmospheric Flight Mechanics Conference, AIAA 2003-5397, AIAA Washington, DC, 2003.
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Analysis of Wind Tunnel Lateral Oscillatory Data of the F-16XL Aircraft
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Vladislav, K.1
Murphy, P.C.2
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19644394112
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Mathematical modeling of aircraft unsteady aerodynamics at high incidence with account of wing-tail interaction
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AIAA Washington, DC
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Khrabrov, A.1
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Abromov, N.3
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33751413276
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Estimation of longitudinal unsteady aerodynamics of a wing-tail combination from wind tunnel data
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AIAA Washington, DC
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Murphy Patrick, C.1
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19644364148
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Progressive aerodynamic model identification from dynamic water tunnel test of the F-16XL aircraft
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AIAA Washington, DC
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Murphy, Patrick C, Klein, Vladislav, and Szyba, Nathan M., "Progressive Aerodynamic Model Identification from Dynamic Water Tunnel Test of the F-16XL Aircraft, " AIAA Atmospheric Flight Mechanics Conference, AIAA 2004-5277, AIAA Washington, DC, 2004.
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Murphy, P.C.1
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