Flight flutter testing and aeroelastic stability of aircraft

Date

2007-03-01

Author

Kayran, Altan

Metadata

Show full item record

This work is licensed under a Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.

Item Usage Stats

95
views

0
downloads

URI

https://hdl.handle.net/11511/93004

Journal

Aircraft Engineering And Aerospace Technology

Collections

Department of Aerospace Engineering, Article

Suggestions

OpenMETU
Core

Flight flutter testing and aeroelastic stability of aircraft Kayran, Altan (2007-01-01) Purpose - To provide a general review of the flight flutter test techniques utilized in aeroelastic stability flight testing of aircraft, and to highlight the key items involved in flight flutter testing of aircraft, by emphasizing all the main information processed during the flutter stability verification based on flight test data.
Flight flutter testing and aeroelastic stability of aircraft Kayran, Altan (2007-01-01) Purpose - This paper sets out to provide a general review of the flight flutter test techniques utilized in aeroelastic stability flight testing of aircraft, and to highlight the key items involved in flight flutter testing of aircraft, by emphasizing all the main information processed during the flutter stability verification based on flight test data.
Flight test maneuver design and aerodynamic parameter estimation for single use autonomous air vehicles Vefa Yavuzturk, N.; Topbas, Eren; Yazıcıoğlu, Yiğit (null; 2017-01-01) In this paper, a maneuver design and aerodynamic parameter estimation procedure is carried out for single use autonomous gliding air vehicles where allowable flight testing time is limited. At first, using the priori aerodynamics of a gliding vehicle, an aerodynamic model has been built and six degree of freedom simulation tool is generated. This priori aerodynamic knowledge is used to design a multi-sine input to excite the system at predetermined flight conditions during flight test. Afterwards, using the...
Flight simulation and control of a helicopter Erçin, Gülsüm Hilal; Tekinalp, Ozan; Department of Aerospace Engineering (2008) In this thesis the development of a nonlinear simulation model of a utility helicopter and the design of its automatic flight control system is addressed. In the first part of this thesis, the nonlinear dynamic model for a full size helicopter is developed using the MATLAB/SIMULINK environment. The main rotor (composed of inflow and flapping dynamics parts), tail rotor, fuselage, vertical stabilizer, horizontal stabilizer of the helicopter are modeled in order to obtain the total forces and moments needed f...
Flight control using neural networks and fuzzy logic Erinmez, Mehmet Özgür; Leblebicioğlu, Kemal; Department of Electrical and Electronics Engineering (1997)

Citation Formats

A. Kayran, “Flight flutter testing and aeroelastic stability of aircraft,” Aircraft Engineering And Aerospace Technology, vol. 79, no. 2, pp. 150–162, 2007, Accessed: 00, 2021. [Online]. Available: https://hdl.handle.net/11511/93004.