Zobrazeno 1 - 10
of 12
pro vyhledávání: '"Goman, M. (Mikhail G.)"'
The file attached to this record is the author's final peer reviewed version. The high-incidence aerodynamics of a lightweight jet trainer aircraft model has been investigated using a novel five-degree-of-freedom (DOF) dynamic maneuver rig, recently
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::b2c700949c19a48b8d0ca51212a82394
https://doi.org/10.2514/1.c034995
https://doi.org/10.2514/1.c034995
Computational Ground Effect Aerodynamics and Airplane Stability Analysis During Take-off and Landing
Computational simulations of aerodynamic characteristics of the Common Research Model (CRM), representing a typical transport airliner, are conducted using CFD methods in close proximity to the ground. The obtained dependencies on bank angle for aero
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::ee03df99e2fb4ada0ebdbd7078645432
http://hdl.handle.net/2086/14704
http://hdl.handle.net/2086/14704
Experimental results for aerodynamic static hysteresis at stall conditions obtained in the TsAGI's T-124 low-turbulence wind tunnel for NACA0018 are presented and analysed. Computational predictions of aerodynamic static hysteresis are made using the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::1d76b84be567cc5239b12646a8a2202c
http://hdl.handle.net/2086/14049
http://hdl.handle.net/2086/14049
Flight at high angles of attack is associated with a variety of types of aircraft departure and post stall behaviour. Every aircraft will exhibit specific set of flight characteristics in extended flight envelope. This work was motivated by the need
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::8f55cf9898999d9050dd11abed67aaa4
http://hdl.handle.net/2086/11809
http://hdl.handle.net/2086/11809
There is a significant interest in developing flight control laws which need minimum gain scheduling across the whole flight envelope while providing required robust performance and stability properties to the closed-loop system. Dynamic inversion an
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::82efc939dd2873bb1ae17c8aa6e10f2c
http://hdl.handle.net/2086/9106
http://hdl.handle.net/2086/9106
An active flutter suppression using linear sub-optimal control scheme is investigated for a 2dof airfoil system with nonlinear torsional stiffness and limited deflection amplitude of its single actuator. The suppression of limit cycle oscillations in
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::1bdffa41205505d010b87fb1431de1a8
http://hdl.handle.net/2086/9103
http://hdl.handle.net/2086/9103
An active stabilization of flutter instability was investigated using mathematical model for two degree-of freedom aeroelastic airfoil system with trailing and leading edge flaps. A number of control laws based on LQR, linear eigenstructure assignmen
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::6dc65151cf0c04a66121034d74623901
http://hdl.handle.net/2086/9100
http://hdl.handle.net/2086/9100
The effect of amplitude and rate control constraints in active flutter suppression was analysed for a number of different linear and nonlinear control laws considering mathematical model of two degree-of freedom aeroelastic airfoil system with traili
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::1b5fd69ebd7006d4bb4955a25a105949
http://hdl.handle.net/2086/9102
http://hdl.handle.net/2086/9102
Autor:
Groen, E., Wentink, M., Mayrhofer, Michael, Smaili, H., Soemarwoto, B., Goman, M. (Mikhail G.), Bulthoff, H.H.
The collaborative research project SUPRA, intends to develop methodologies and advanced flight simulator concepts for teaching airline pilots to detect, and recover from adverse flight upsets that lead to unusual attitudes. The project is funded by t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::769d1af98500f45f1eaa4b1de6eb601c
http://hdl.handle.net/2086/9110
http://hdl.handle.net/2086/9110