Development of a wing preliminary structural analysis code.

Dinçer, Süha Özgür


Development of a Wing Preliminary Structural Analysis code
Yaman, Yavuz (American Institute of Aeronautics and Astronautics (AIAA), 2002-05-01)
Development of a flexible satellite simulator and associated control algorithms.
Taylan, Koray; Tekinalp, Ozan; Department of Aeronautical Engineering (2002)
Development of a PC-based partial discharge detection and measurement system.
Taşcı, Alper; Hızal, Mirzahan; Department of Electrical and Electronics Engineering (2002)
Development of forward flight trim and longitudinal dynamic stability codes and their application to a uh-60 helicopter
Çalışkan, Sevinç; Özyörük, Yusuf; Department of Aerospace Engineering (2009)
This thesis describes the development of a series of codes for trim and longitudinal stability analysis of a helicopter in forward flight. In general, particular use of these codes can be made for parametric investigation of the effects of the external and internal systems integrated to UH-60 helicopters. However, in this thesis the trim analysis results are obtained for a clean UH-60 configuration and the results are compared with the flight test data that were acquired by ASELSAN, Inc. The first of the de...
Development of a computer program for ultimate strength of rectangular steel box girders.
Uykur, A. Berkhan; Department of Civil Engineering (1985)
Citation Formats
S. Ö. Dinçer, “Development of a wing preliminary structural analysis code.,” Middle East Technical University, 2000.