Measurement of lift and drag in morphing wings using a high precision load cell

Download
2015
Özkanaktı, Mehmet Harun
This thesis focuses on computational and experimental investigation of three different morphing wing planforms and a baseline wing planform using a commercial CFD software and load cell measurements for the validation of an optimization code developed in a separate study. The wing planforms of interest originate from an optimization tool that minimizes drag for a constant value of lift at a given velocity. The first planform of interest is the planform for optimized drag subject to 14 m/s freestream velocity with constraints for physical dimensions and taper ratio. The other two planforms are generated using the first planform as baseline and optimizing the drag with constant lift subjected to 10 m/s and 16.5 m/s freestream velocity, respectively. In this optimization part, airfoil physical thickness allowances are introduced as inequality constraints to the optimization process. For every case, each of the wing planforms are analyzed by a CFD software and tested with load cell measurements for the corresponding freestream velocity. The results of these analyses and experiments are used to extract lift and drag forces for a wide range of angles of attack. Relations between these parameters and drag of the optimized wing planforms are established in order to validate the optimization code. Final deduction of aerodynamic parameters ensures that the code that has been developed for the optimization of morphing wing planforms for different flight conditions is valid and useful.

Suggestions

Measurement of Lift and Drag Force in Morphing Wings Using High Precision Load Cell
Özkanaktı, Harun; Körpe, Durmuş Sinan; Özgen, Serkan (2015-06-29)
This study focuses on experimental investigation of three different morphing wing planforms and a baseline wing planform using commercial CFD software and load cell measurements in a wind tunnel for the validation of an optimization code developed separately [1]. The wing planforms of interest originate from an optimization code that minimizes drag for a required lift utilizing a 3-D panel method with a 2-D boundary layer solver. The optimization method is gradient based. The first planform of interest is t...
Aerodynamic modelling and optimization of morphing wings
Körpe, Durmuş Sinan; Özgen, Serkan; Department of Aerospace Engineering (2014)
This thesis deals with aerodynamic optimization of morphing wings under performance and geometric constraints. In order to perform the optimization process, flow solvers computing aerodynamic lift and drag were developed as a function evaluator. A gradient based optimization method was used in order to develop the optimization algorithm. Three dimensional panel method solver was developed in order to obtain lift, pressure drag and induced drag values for a finite wing. Obtained results were compared with di...
Implementation of turbulence models on 2d hybrid grids using an explicit/implicit multigrid algorithm
Yılmaz, Ali Emre; Tuncer, İsmail Hakkı; Department of Aerospace Engineering (2011)
In this thesis study, implementation, numerical stability and convergence rate issues of turbulence modeling are explored. For this purpose, a one equation turbulence model, Spalart-Allmaras, and a two-equation turbulence model, SST k-w, are adapted to an explicit, cell centered, finite volume method based, structured / hybrid multi grid flow solver, SENSE2D, developed at TUBITAK-SAGE. Governing equations for both the flow and the turbulence are solved in a loosely coupled manner, however, each set of equat...
Description and performance of track and primary-vertex reconstruction with the CMS tracker
Chatrchyan, S.; et. al. (IOP Publishing, 2014-10-01)
A description is provided of the software algorithms developed for the CMS tracker both for reconstructing charged-particle trajectories in proton-proton interactions and for using the resulting tracks to estimate the positions of the LHC luminous region and individual primary-interaction vertices. Despite the very hostile environment at the LHC, the performance obtained with these algorithms is found to be excellent. For t (t) over bar events under typical 2011 pileup conditions, the average track-reconstr...
Reconstruction and identification of tau lepton decays to hadrons and nu(tau) at CMS
Khachatryan, V.; et. al. (IOP Publishing, 2016-01-01)
This paper describes the algorithms used by the CMS experiment to reconstruct and identify tau -> hadrons + nu(tau) decays during Run 1 of the LHC. The performance of the algorithms is studied in proton-proton collisions recorded at a centre-of-mass energy of 8 TeV, corresponding to an integrated luminosity of 19.7 fb(-1). The algorithms achieve an identification efficiency of 50-60%, with misidentification rates for quark and gluon jets, electrons, and muons between per mille and per cent levels.
Citation Formats
M. H. Özkanaktı, “Measurement of lift and drag in morphing wings using a high precision load cell,” M.S. - Master of Science, Middle East Technical University, 2015.