Show/Hide Menu
Hide/Show Apps
Logout
Türkçe
Türkçe
Search
Search
Login
Login
OpenMETU
OpenMETU
About
About
Open Science Policy
Open Science Policy
Open Access Guideline
Open Access Guideline
Postgraduate Thesis Guideline
Postgraduate Thesis Guideline
Communities & Collections
Communities & Collections
Help
Help
Frequently Asked Questions
Frequently Asked Questions
Guides
Guides
Thesis submission
Thesis submission
MS without thesis term project submission
MS without thesis term project submission
Publication submission with DOI
Publication submission with DOI
Publication submission
Publication submission
Supporting Information
Supporting Information
General Information
General Information
Copyright, Embargo and License
Copyright, Embargo and License
Contact us
Contact us
Flow and Noise Prediction of Doors-on M219 Cavity through Improved Delayed Detached Eddy Simulations
Date
2019-05-14
Author
Coşkun, Seyfettin
Özyörük, Yusuf
Metadata
Show full item record
Item Usage Stats
440
views
0
downloads
Cite This
High survivability and low observability requirements of modern fighter airplanes necessitate internal carriage of the stores. During their deployment the doors of internal weapon bays are opened transitionally, forming a cavity and hence a highly unsteady and nonlinear flow coupled with acoustic feedback mechanism. These processes present unsteady vibratory loads on the stores and structures. In the present paper, CFD computations of the doors-on M219 cavity with use of Improved Delayed Detached Eddy Simulation (IDDES) are carried out to predict the turbulent fluctuations and the associated noise. Computationally less expensive Unsteady Reynolds-Averaged NavierStokes (URANS) calculations with kω-SST model are also carried out. Comparisons of the attained overall sound pressure levels at various locations on the cavity ceiling with experimental data show the latter approach usually lacks accuracy with overpredicted values, while the former one predicts the levels quite well.
URI
https://hdl.handle.net/11511/75603
http://www.parcfd.org/2019/program/serv.php?No=1090
Conference Name
31st International Conference on Parallel Computational Fluid Dynamics, (14 - 17 Mayıs 2019)
Collections
Department of Aerospace Engineering, Conference / Seminar
Suggestions
OpenMETU
Core
Turbulent flow and acoustic predictions over open cavity configurations at transonic speeds
Çoşkun, Seyfettin.; Özyörük, Yusuf; Department of Aerospace Engineering (2019)
In modern military fighters, internal carriage of weapons is vital in terms of high survivability, low observability and aerodynamic performance of the fighter. During store release phases of operation, the aircraft will have to fly with the cavity exposed to free stream conditions. When an aircraft internal weapons bay is exposed to free stream of air, a highly unsteady and complex flow field develops within the cavity. This triggers intense aero-acoustic environment in and around the cavity. Highly complex, un...
ADJOINT-BASED AERODYNAMIC SHAPE OPTIMIZATION OF A STRAKE-DELTA WING CONFIGURATION
Yutük, Kaan; Tuncer, İsmail Hakkı; Department of Aerospace Engineering (2021-11-8)
Modern fighter aircraft compulsorily demand high maneuverability capability, which is mainly provided by an improved aerodynamic performance at high angles of attack. This is achieved by mostly employing strakes and canards. In this study, adjoint-based configuration and leading edge shape optimizations of a strake on a double-delta wing configuration are performed. SU2 is employed for flow and adjoint solutions. SU2 flow solutions are first verified on solutions for adaptive grids. In the configuration opt...
DYNAMIC MODELING AND CONTROL OF AN ELECTROMECHANICAL CONTROL ACTUATION SYSTEM
Yerlikaya, Umit; Balkan, Raif Tuna (2017-10-13)
Electromechanical actuators are widely used in miscellaneous applications in engineering such as aircrafts, missiles, etc. due to their momentary overdrive capability, long-term storability, and low quiescent power/low maintenance characteristics. This work focuses on electromechanical control actuation systems (CAS) that are composed of a brushless direct current motor, ball screw, and lever mechanism. In this type of CAS, nonlinearity and asymmetry occur due to the lever mechanism itself, saturation limit...
Structured H-Infinity controller design and analysis for highly maneuverable jet aircraft
Özkan, Salih Volkan; Tekinalp, Ozan; Department of Aerospace Engineering (2022-2-10)
Robust control technique is utilized to develop flight control laws for highly maneuverable aircraft. A structured H-Infinity controller is used to optimize the gains of the proposed control algorithm. For this purpose systune algorithm available in Matlab is employed to successfully obtain the controller gains satisfying selected design requirements. Designed control laws are evaluated according to these requirements and validation of the methodology is presented.
FREQUENCY-DOMAIN SYSTEM IDENTIFICATION OF F-16 LONGITUDINAL DYNAMICS
Ergazi, Nazife Ege; Yavrucuk, İlkay; Gürsoy, Gönenç; Department of Aerospace Engineering (2022-3-10)
The longitudinal dynamics of F-16 aircraft in a level trim, unaccelerated flight are identified using frequency-domain system identification techniques. The nonlinear system is excited by sine sweep elevator input, and angle of attack and pitch rate responses are collected. Detrending and windowing are applied to time-domain data and are converted to the frequency-domain by applying Fast Fourier Transform (FFT). The smooth spectral estimates are found from the transformed data, allowing frequency responses ...
Citation Formats
IEEE
ACM
APA
CHICAGO
MLA
BibTeX
S. Coşkun and Y. Özyörük, “Flow and Noise Prediction of Doors-on M219 Cavity through Improved Delayed Detached Eddy Simulations,” presented at the 31st International Conference on Parallel Computational Fluid Dynamics, (14 - 17 Mayıs 2019), Antalya, Türkiye, 2019, Accessed: 00, 2021. [Online]. Available: https://hdl.handle.net/11511/75603.