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Kozakiewicz, Adam
in Cooperation with on an Cooperation-Score of 37%
Topics
- aircraft
- turbine
- compressor
- air intake
- turbine engine
- assessment
- modeling
- simulation
- airport
- duct
- pressure
- propeller blade
- airplane
- stator
- jet propelled aircraft
- engine operation
- numerical analysis
- vortex
- jet engine
- surging
- stall
- pressure field
- propulsion
- weapon
- optimisation
- airfoil
- drone
- vibration
- aerodynamic
- examination
- fuselage
- gust
- engineering
- engine
- show 4 more
Publications (13/13 displayed)
- 2022Areas of Investigation into Air Intake Systems for the Impact on Compressor Performance Stability in Aircraft Turbine Enginescitations
- 2022Determination of Ranges of Unstable Operation of Axial Compressor for Aircraft Turbine Engines
- 2022Intake System Performance Stability as a Function of Flow Throttling
- 2021ELECTRIC AIRCRAFT PROPULSION
- 2018Main problems of the evaluation and selection of advanced weapon systems exemplified by a multi-role combat aircraftcitations
- 2016A unified method of identification and optimization of airfoils for aircrafts, turbine and compressor blades
- 2015Modeling of an Unmanned Aerial Vehicle (UAV) Body for the Needs of Numerical Aerodynamic Investigations, Strength Analysis and Examinations of Free Vibrationscitations
- 2015Modeling of an Unmanned Aerial Vehicle (UAV) Body for the Needs of Numerical Aerodynamic Investigations, Strenght Analysis and Examinations of Free Vibrationscitations
- 2013Analysis Of The Gust Impact On Inlet Vortex Formation Of The Fuselage-Shielded Inlet Of An Jet Engine Powered Aircraft
- 2013Application of CAD/CAM/CAE Systems to the Process of Aircraft Structures Analysis by Means of Reverse Engineering Methods
- 2013Unified Method of Identification and Optimization of Airfoils for Aircrafts, Turbine and Compressor Blades
- 2013Unstable operation of the turbine aircraft engine
- 2011Construction of an air intake system model for F-100-PW-229 engine in F-16 aircraft for intake vortex development analysis
Places of action
article
Modeling of an Unmanned Aerial Vehicle (UAV) Body for the Needs of Numerical Aerodynamic Investigations, Strength Analysis and Examinations of Free Vibrations
Topics
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