M
Mikhail Goman
Researcher at De Montfort University
Publications - 65
Citations - 1252
Mikhail Goman is an academic researcher from De Montfort University. The author has contributed to research in topics: Aerodynamics & Wind tunnel. The author has an hindex of 14, co-authored 59 publications receiving 1093 citations.
Papers
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State-Space Representation of Aerodynamic Characteristics of an Aircraft at High Angles of Attack
Mikhail Goman,A. N. Khrabrov +1 more
TL;DR: In this article, the state-space representation of aerodynamic forces and moments for unsteady aircraft motion is proposed, considering separated flow about an airfoil and flow with vortex breakdown about a slender delta wing gives the base for mathematical modeling using internal variables describing the flow state.
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Application of bifurcation methods to nonlinear flight dynamics problems
TL;DR: In this paper, applications of global stability and bifurcational analysis methods are presented for different nonlinear flight dynamics problems, such as roll-coupling, stall, spin, etc.
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Evaluation of Aircraft Performance and Maneuverability by Computation of Attainable Equilibrium Sets
TL;DR: In this article, a systematic way of computing the set of all attainable steady states for a general class of helical trajectories is presented, and the proposed reconstruction of attainable equilibrium states and their local stability maps provides a comprehensive and consistent representation of the aircraft flight and maneuvering envelopes.
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Application of continuation and bifurcation methods to the design of control systems
Mikhail Goman,A. V. Khramtsovsky +1 more
TL;DR: The nonlinear control law, which totally suppresses wing-rock motion, is derived, taking into account both local stability characteristics of aircraft equilibrium states and domains of attraction, along with the requirement that all other attractors be eliminated.
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Multi-Degree-of-Freedom Wind-Tunnel Maneuver Rig for Dynamic Simulation and Aerodynamic Model Identification
TL;DR: In this paper, a five-degree-of-freedom rig for the dynamic wind-tunnel testing of aircraft models has been developed, which enables a large set of conventional and more-extreme aircraft maneuvers to be performed in the controlled environment of a wind tunnel, allowing direct physical simulation of in-flight maneuvers and the identification of aerodynamic models from aircraft-model time histories.