| High altitude long endurance unmanned aerial vehicle of a new generation–a design challenge for a low cost, reliable and high performance aircraft Z Goraj, A Frydrychewicz, R Świtkiewicz, B Hernik, J Gadomski, ... Bulletin of the Polish Academy of Sciences Technical Sciences, 173-194-173-194, 2004 | 53 | 2004 |
| Flutter calculation based on GVT‐results and theoretical mass model W Chajec Aviation 13 (4), 122-129, 2009 | 17 | 2009 |
| Aeroelastic analysis of remotely controlled research vehicles with numerous control surfaces Z Goraj, W Chajec International Journal of Structural Integrity 2 (2), 158-184, 2011 | 6 | 2011 |
| Aeroelastic analyses in “PZL-Mielec” using MSC/NASTRAN W Chajec 1999 MSC Worldwide Aerospace Conference, Long Beach, CA. http://web …, 1999 | 6 | 1999 |
| Comparison of flutter calculation methods based on ground vibration test result W Chajec Aircraft Engineering and Aerospace Technology 91 (3), 466-476, 2018 | 5 | 2018 |
| CRITICAL FLUTTER SPEED OF SAILPLANES CALCUTATED FOR HIGH ALTITUDE: EXAMPLES OF COMPUTATION W Chajec Technical Soaring 18 (3), 67-72, 1993 | 5 | 1993 |
| Methods of modern aircraft aeroelastic analyses in the institute of aviation W Chajec Journal of KONES 25 (4), 33-42, 2018 | 4 | 2018 |
| Modal approach in the fluid-structure interaction in aerospace W Chajec, A Dziubiński Advances in Mechanics: Theoretical, Computational and Interdisciplinary …, 2015 | 4 | 2015 |
| Fluid structure interaction for symmetric manoeuvre base on ultra light plane R Roszak, W Stankiewicz, M Morzyński, W Chajec AIP Conference Proceedings 1389 (1), 86-89, 2011 | 3 | 2011 |
| Flutter Computation Based on Ground Vibration Test Results and Mass Data W Chajec Advances in Engineering Research 12, Chapter 5, 2016 | 2 | 2016 |
| Obliczenia flatteru prostokątnego płata ze sterem za pomocą MSC NASTRAN, ZONA ZAERO i ANSYS/Fluent-porównanie z wynikami badań w tunelu aerodynamicznym W Chajec, A Dziubiński Prace Instytutu Lotnictwa, 2016 | 2 | 2016 |
| Flutter Analysis During the Design of sailplanes W Potkanski, W Chajec Technical Soaring 13 (4), 135-140, 1989 | 2 | 1989 |
| Flutter analysis of gliders W Chajec, W Potkanski OSTIV Publications 18, 1985 | 2 | 1985 |
| The effect of wing-tip propulsors on Icaré 2 aeroelasticity W Chajec, WA Krzymien, A Strohmayer Aircraft Engineering and Aerospace Technology 91 (3), 509-524, 2018 | 1 | 2018 |
| Aeroelastic Calculation of Innovative Non-conventional Aircraft with Swinging Canard Surface WC Chajec Journal of Aeroelasticity and Structural Dynamics 3 (1), 2014 | 1 | 2014 |
| Aeroelastic Simulation for Symmetric Manoeuvre of I23 Manager Light Plane R Roszak, W Stankiewicz, M Morzynski, W Chajec Journal of Physical Science and Application 2 (8), 274, 2012 | 1 | 2012 |
| Wykorzystanie pomiarów rezonansowych do analizy flatteru samolotu po zmianie rozkładu masy W Chajec Politechnika Warszawska, 2011 | 1 | 2011 |
| Przegląd metod obliczeniowej analizy flatteru na przykładzie samolotu I-23 W Chajec Prace Instytutu Lotnictwa, 20-34, 2011 | 1 | 2011 |
| Consideration of mass elements of the control system in a flutter analysis(Uwzglednianie mas elementow ukladu sterowania w obliczeniach flatteru) W CHAJEC Instytut Lotnictwa, Prace, 77-90, 1993 | | 1993 |
| Osiowosymetryczny opływ układu pierścieni cieczą doskonałą W Chajec Zeszyty Naukowe Instytutu Maszyn Przepływowych Polskiej Akademii Nauk w …, 1983 | | 1983 |
Marcin FigatWarsaw University of TechnologyVerified email at meil.pw.edu.pl
