國立虎尾科技大學 |

Time-averaged surrogate modeling for small scale propellers based on high-fidelity CFD simulations

紀錄類型:	書目-語言資料,印刷品 : Monograph/item
正題名/作者:	Time-averaged surrogate modeling for small scale propellers based on high-fidelity CFD simulations/ Joseph Ray Carroll.
作者:	Carroll, Joseph Ray,
面頁冊數:	1 electronic resource (190 pages)
附註:	Source: Dissertations Abstracts International, Volume: 75-07, Section: B.
Contained By:	Dissertations Abstracts International75-07B.
標題:	Mechanical engineering. -
電子資源:	http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=3603422
ISBN:	9781303580338

Time-averaged surrogate modeling for small scale propellers based on high-fidelity CFD simulations
Carroll, Joseph Ray,

Time-averaged surrogate modeling for small scale propellers based on high-fidelity CFD simulations [electronic resource] /Joseph Ray Carroll. - 1 electronic resource (190 pages)

Source: Dissertations Abstracts International, Volume: 75-07, Section: B.

Many Small Unmanned Aerial Vehicles (SUAV) are driven by small scale, fixed blade propellers. The flow produced by the propeller, known as the propeller slipstream, can have significant impact on SUAV aerodynamics. In the design and analysis process for SUAVs, numerous Computational Fluid Dynamic (CFD) simulations of the coupled aircraft and propeller are often conducted which require a time-averaged, steady-state approximation of the propeller for computational efficiency. Most steady-state propeller models apply an actuator disk of momentum sources to model the thrust and swirl imparted to the flow field by a propeller. These momentum source models are based on simplified theories which lack accuracy. Currently, the most common momentum source models are based on blade element theory. Blade element theory discretizes the propeller blade into airfoil sections and assumes them to behave as two-dimensional (2D) airfoils. Blade element theory neglects many 3D flow effects that can greatly affect propeller performance limiting its accuracy and range of application. The research work in this dissertation uses a surrogate modeling method to develop a more accurate momentum source propeller model. Surrogate models for the time averaged thrust and swirl produced by each blade element are trained from a database of time-accurate, high-fidelity 3D CFD propeller simulations. Since the surrogate models are trained from these high-fidelity CFD simulations, various 3D effects on propellers are inherently accounted for such as tip loss, hub loss, post stall effect, and element interaction. These efficient polynomial response surface surrogate models are functions of local flow properties at the blade elements and are embedded into 3D CFD simulations as locally adaptive momentum source terms. Results of the radial distribution of thrust and swirl for the steady-state surrogate propeller model are compared to that of time-dependent, high-fidelity 3D CFD propeller simulations for various aircraft-propeller coupled situations. This surrogate propeller model which is dependent on local flow field properties simulates the time-averaged flow field produced by the propeller at a momentum source term level of detail. Due to the nature of the training cases, it also captures the accuracy of time dependent 3D CFD propeller simulations but at a much lower cost.

English

ISBN: 9781303580338Subjects--Topical Terms:

557493
Mechanical engineering.
Subjects--Index Terms:

Blade

Time-averaged surrogate modeling for small scale propellers based on high-fidelity CFD simulations
LDR:03964nam a22004453i 4500 001 1172964
005 20260622113210.5
006 m o d
007 cr|nu||||||||
008 260803s2013 miu||||||m |||||||eng d
020 $a 9781303580338
035 $a (MiAaPQD)AAI3603422
035 $a (MiAaPQD)msstate:11710
035 $a AAI3603422
040 $a MiAaPQD $b eng $c MiAaPQD $e rda
100 1 $a Carroll, Joseph Ray, $e author. $3 1503616
245 1 0 $a Time-averaged surrogate modeling for small scale propellers based on high-fidelity CFD simulations $c Joseph Ray Carroll. $h [electronic resource] /
264 1 $a Ann Arbor : $b ProQuest Dissertations & Theses, $c 2013
300 $a 1 electronic resource (190 pages)
336 $a text $b txt $2 rdacontent
337 $a computer $b c $2 rdamedia
338 $a online resource $b cr $2 rdacarrier
500 $a Source: Dissertations Abstracts International, Volume: 75-07, Section: B.
500 $a Publisher info.: Dissertation/Thesis.
500 $a Advisors: Marcum, David L. Committee members: Janus, J. M.; Thompson, D. S.; Walters, D. K.
502 $b Ph.D. $c Mississippi State University $d 2013.
520 # $a Many Small Unmanned Aerial Vehicles (SUAV) are driven by small scale, fixed blade propellers. The flow produced by the propeller, known as the propeller slipstream, can have significant impact on SUAV aerodynamics. In the design and analysis process for SUAVs, numerous Computational Fluid Dynamic (CFD) simulations of the coupled aircraft and propeller are often conducted which require a time-averaged, steady-state approximation of the propeller for computational efficiency. Most steady-state propeller models apply an actuator disk of momentum sources to model the thrust and swirl imparted to the flow field by a propeller. These momentum source models are based on simplified theories which lack accuracy. Currently, the most common momentum source models are based on blade element theory. Blade element theory discretizes the propeller blade into airfoil sections and assumes them to behave as two-dimensional (2D) airfoils. Blade element theory neglects many 3D flow effects that can greatly affect propeller performance limiting its accuracy and range of application. The research work in this dissertation uses a surrogate modeling method to develop a more accurate momentum source propeller model. Surrogate models for the time averaged thrust and swirl produced by each blade element are trained from a database of time-accurate, high-fidelity 3D CFD propeller simulations. Since the surrogate models are trained from these high-fidelity CFD simulations, various 3D effects on propellers are inherently accounted for such as tip loss, hub loss, post stall effect, and element interaction. These efficient polynomial response surface surrogate models are functions of local flow properties at the blade elements and are embedded into 3D CFD simulations as locally adaptive momentum source terms. Results of the radial distribution of thrust and swirl for the steady-state surrogate propeller model are compared to that of time-dependent, high-fidelity 3D CFD propeller simulations for various aircraft-propeller coupled situations. This surrogate propeller model which is dependent on local flow field properties simulates the time-averaged flow field produced by the propeller at a momentum source term level of detail. Due to the nature of the training cases, it also captures the accuracy of time dependent 3D CFD propeller simulations but at a much lower cost.
546 $a English
590 $a School code: 0132
650 # 4 $a Mechanical engineering. $3 557493
653 # # $a Blade
653 # # $a Computational fluid dynamic
653 # # $a Element
653 # # $a Momentum
653 # # $a Propeller
653 # # $a Surrogate
690 $a 0548
710 2 # $a Mississippi State University. $b Mechanical Engineering. $3 845713
720 1 $a Marcum, David L. $e degree supervisor.
773 0 # $t Dissertations Abstracts International $g 75-07B.
790 $a 0132
791 $a Ph.D.
792 $a 2013
856 4 0 $u http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=3603422