Page 1 | Search Results | Aircraft Engineering and Aerospace Technology: An International Journal

1-8 of 8

Sort by

Sort Order Select

Journal Articles

Flight dynamics models used in different national and international projects

Zdobyslaw Goraj

Aircraft Engineering and Aerospace Technology: An International Journal (2014) 86 (3): 166–178.

https://doi.org/10.1108/AEAT-02-2013-0036

Published: 29 April 2014

View article titled, Flight dynamics models used in different national and international projects

Add to Citation Manager for Flight dynamics models used in different national and international projects

Journal Articles

MALE UAV design of an increased reliability level

Tomasz Goetzendorf‐Grabowski, Andrzej Frydrychewicz, Zdobysław Goraj, Stanisław Suchodolski

Aircraft Engineering and Aerospace Technology: An International Journal (2006) 78 (3): 226–235.

https://doi.org/10.1108/17488840610663693

Published: 01 May 2006

View article titled, MALE UAV design of an increased reliability level

Add to Citation Manager for MALE UAV design of an increased reliability level

Journal Articles

Analysis and optimisation of a MALE UAV loaded structure

Jacek Gadomski, Bogdan Hernik, Zdobyslaw Goraj

Aircraft Engineering and Aerospace Technology: An International Journal (2006) 78 (2): 120–131.

https://doi.org/10.1108/17488840610653423

Published: 01 March 2006

View article titled, Analysis and optimisation of a MALE UAV loaded structure

Add to Citation Manager for Analysis and optimisation of a MALE UAV loaded structure

Journal Articles

Aerodynamic calculation of unmanned aircraft

Marcin Figat, Tomasz Goetzendorf‐Grabowski, Zdobysław Goraj

Aircraft Engineering and Aerospace Technology: An International Journal (2005) 77 (6): 467–474.

https://doi.org/10.1108/00022660510628453

Published: 01 December 2005

View article titled, Aerodynamic calculation of unmanned aircraft

Add to Citation Manager for Aerodynamic calculation of unmanned aircraft

Journal Articles

Design challenges associated with development of a new generation UAV

Zdobysław Goraj

Aircraft Engineering and Aerospace Technology: An International Journal (2005) 77 (5): 361–368.

https://doi.org/10.1108/00022660510617086

Published: 01 October 2005

View article titled, Design challenges associated with development of a new generation UAV

Add to Citation Manager for Design challenges associated with development of a new generation UAV

Journal Articles

Experimental and numerical results obtained for a scaled RPV and a full size aircraft

Cezary Galinski, Zdobyslaw Goraj

Aircraft Engineering and Aerospace Technology: An International Journal (2004) 76 (3): 305–313.

https://doi.org/10.1108/00022660410536041

Published: 01 June 2004

View article titled, Experimental and numerical results obtained for a scaled RPV and a full size aircraft

Add to Citation Manager for Experimental and numerical results obtained for a scaled RPV and a full size aircraft

Journal Articles

Dynamics of a light aircraft in spin

Zdobysław Goraj, Alfred Baron, Jan Kacprzyk

Aircraft Engineering and Aerospace Technology: An International Journal (2002) 74 (3): 237–251.

https://doi.org/10.1108/00022660210427422

Published: 01 June 2002

View article titled, Dynamics of a light aircraft in spin

Add to Citation Manager for Dynamics of a light aircraft in spin

Journal Articles

Extreme loads acting on transport airplane following a sudden change in symmetric equilibrium

Zdobyslaw Goraj, Janusz Sznajder

Aircraft Engineering and Aerospace Technology: An International Journal (2002) 74 (2): 125–137.

https://doi.org/10.1108/00022660210420834

Published: 01 April 2002

View article titled, Extreme loads acting on transport airplane following a sudden change in symmetric equilibrium

Add to Citation Manager for Extreme loads acting on transport airplane following a sudden change in symmetric equilibrium

Update search

NARROW

Format

Journal

Type

Date

Availability

Flight dynamics models used in different national and international projects

MALE UAV design of an increased reliability level

Analysis and optimisation of a MALE UAV loaded structure

Aerodynamic calculation of unmanned aircraft

Design challenges associated with development of a new generation UAV

Experimental and numerical results obtained for a scaled RPV and a full size aircraft

Dynamics of a light aircraft in spin

Extreme loads acting on transport airplane following a sudden change in symmetric equilibrium

Email alerts