본문

서브메뉴

Analysis and Prediction of the Rigid, Coaxial Rotor System's Blade-crossover Interaction Events
Analysis and Prediction of the Rigid, Coaxial Rotor System's Blade-crossover Interaction E...
Analysis and Prediction of the Rigid, Coaxial Rotor System's Blade-crossover Interaction Events

상세정보

자료유형  
 학위논문 서양
최종처리일시  
20260202105320
ISBN  
9798297671645
DDC  
330
저자명  
Sharma, Kalki.
서명/저자  
Analysis and Prediction of the Rigid, Coaxial Rotor Systems Blade-crossover Interaction Events
발행사항  
[Sl] : The Pennsylvania State University, 2025
발행사항  
Ann Arbor : ProQuest Dissertations & Theses, 2025
형태사항  
289 p
주기사항  
Source: Dissertations Abstracts International, Volume: 87-04, Section: B.
주기사항  
Advisor: Brentner, Kenneth S.
학위논문주기  
Thesis (Ph.D.)--The Pennsylvania State University, 2025.
초록/해제  
요약The modern compound coaxial helicopter, such as the Raider and Defiant, has been developed to overcome the speed limitations of the conventional single main and tail rotor helicopter. Although there are advantages to this configuration, the proximity of the rotors results in aerodynamic interactions between the rotors that cause impulsive loading events, and this results in potential problems with vibrations and acoustics. One of the primary impulsive loading event is the blade-crossover interaction (BCI).This work focuses on understanding, isolating, and predicting BCI events in rigid coaxial rotor systems. BCI events are significant aerodynamic interactions that occur when the blades of the upper and lower rotors cross each other, leading to impulsive loading and increased noise levels. The impact of BCI events is demonstrated through acoustic measurements, with predictions computed using rotor performance data extracted from various analysis tools and fed into acoustic prediction software (PSU-WOPWOP). It is determined that mid-fidelity rotorcraft analysis tools do not adequately account for BCI events, necessitating the use of Computational Fluid Dynamics (CFD). The interaction is also studied in isolation by simulating the crossing of airfoils using approaches of varying fidelity, confirming that lower-order methods fail to capture the physics accounted for in CFD. To compute the BCI events in milliseconds, the data generated from the CFD analysis is used to develop a surrogate model using the Gaussian Process Regression (GPR) model approach. The BCI events are shown to increase sound pressure levels (SPL) by up to 10 dB, effectively doubling noise below the rotor system at high speed forward flight, with the key factors governing the interaction being the speed and vertical separation distance of the rotor blades upon crossover. The key contributions of this work are: 1) demonstrated the importance of BCI events in rotor acoustics, showing that they can add up to 10 dB in SPL; 2) isolated and quantified the impact of BCI events on noise, revealing noise directivity most dominant below and 5° aft of the shaft axis as well as below and parallel to the direction of the BCI events; 3) compared models of varying fidelity, showing that lower-fidelity models over-predict BCI intensity by 2-3 times compared to CFD; 4) developed a surrogate model using 2D CFD data to predict BCI events, providing accurate results at significantly faster computational speeds; 5) showed that appending BCI events to mid-fidelity results improves noise prediction accuracy, bringing it closer to CFD results.
일반주제명  
Aircraft
일반주제명  
Vortices
일반주제명  
Acoustics
일반주제명  
Reynolds number
일반주제명  
Geometry
일반주제명  
Radiation
일반주제명  
Aerodynamics
일반주제명  
Aerospace engineering
일반주제명  
Fluid mechanics
기타저자  
The Pennsylvania State University.
기본자료저록  
Dissertations Abstracts International. 87-04B.
전자적 위치 및 접속  
로그인 후 원문을 볼 수 있습니다.

MARC

 008260126s2025        us                              c    eng  d
■001000017360194
■00520260202105320
■006m          o    d                
■007cr#unu||||||||
■020    ▼a9798297671645
■035    ▼a(MiAaPQ)AAI32289486
■035    ▼a(MiAaPQ)PennState35441kys5232
■040    ▼aMiAaPQ▼cMiAaPQ
■0820  ▼a330
■1001  ▼aSharma,  Kalki.
■24510▼aAnalysis  and  Prediction  of  the  Rigid,  Coaxial  Rotor  System's  Blade-crossover  Interaction  Events
■260    ▼a[Sl]▼bThe  Pennsylvania  State  University▼c2025
■260  1▼aAnn  Arbor▼bProQuest  Dissertations  &  Theses▼c2025
■300    ▼a289  p
■500    ▼aSource:  Dissertations  Abstracts  International,  Volume:  87-04,  Section:  B.
■500    ▼aAdvisor:  Brentner,  Kenneth  S.
■5021  ▼aThesis  (Ph.D.)--The  Pennsylvania  State  University,  2025.
■520    ▼aThe  modern  compound  coaxial  helicopter,  such  as  the  Raider  and  Defiant,  has  been  developed  to  overcome  the  speed  limitations  of  the  conventional  single  main  and  tail  rotor  helicopter.  Although  there  are  advantages  to  this  configuration,  the  proximity  of  the  rotors  results  in  aerodynamic  interactions  between  the  rotors  that  cause  impulsive  loading  events,  and  this  results  in  potential  problems  with  vibrations  and  acoustics.  One  of  the  primary  impulsive  loading  event  is  the  blade-crossover  interaction  (BCI).This  work  focuses  on  understanding,  isolating,  and  predicting  BCI  events  in  rigid  coaxial  rotor  systems.  BCI  events  are  significant  aerodynamic  interactions  that  occur  when  the  blades  of  the  upper  and  lower  rotors  cross  each  other,  leading  to  impulsive  loading  and  increased  noise  levels.  The  impact  of  BCI  events  is  demonstrated  through  acoustic  measurements,  with  predictions  computed  using  rotor  performance  data  extracted  from  various  analysis  tools  and  fed  into  acoustic  prediction  software  (PSU-WOPWOP).  It  is  determined  that  mid-fidelity  rotorcraft  analysis  tools  do  not  adequately  account  for  BCI  events,  necessitating  the  use  of  Computational  Fluid  Dynamics  (CFD).  The  interaction  is  also  studied  in  isolation  by  simulating  the  crossing  of  airfoils  using  approaches  of  varying  fidelity,  confirming  that  lower-order  methods  fail  to  capture  the  physics  accounted  for  in  CFD.  To  compute  the  BCI  events  in  milliseconds,  the  data  generated  from  the  CFD  analysis  is  used  to  develop  a  surrogate  model  using  the  Gaussian  Process  Regression  (GPR)  model  approach.  The  BCI  events  are  shown  to  increase  sound  pressure  levels  (SPL)  by  up  to  10  dB,  effectively  doubling  noise  below  the  rotor  system  at  high  speed  forward  flight,  with  the  key  factors  governing  the  interaction  being  the  speed  and  vertical  separation  distance  of  the  rotor  blades  upon  crossover.  The  key  contributions  of  this  work  are:  1)  demonstrated  the  importance  of  BCI  events  in  rotor  acoustics,  showing  that  they  can  add  up  to  10  dB  in  SPL;  2)  isolated  and  quantified  the  impact  of  BCI  events  on  noise,  revealing  noise  directivity  most  dominant  below  and  5°  aft  of  the  shaft  axis  as  well  as  below  and  parallel  to  the  direction  of  the  BCI  events;  3)  compared  models  of  varying  fidelity,  showing  that  lower-fidelity  models  over-predict  BCI  intensity  by  2-3  times  compared  to  CFD;  4)  developed  a  surrogate  model  using  2D  CFD  data  to  predict  BCI  events,  providing  accurate  results  at  significantly  faster  computational  speeds;  5)  showed  that  appending  BCI  events  to  mid-fidelity  results  improves  noise  prediction  accuracy,  bringing  it  closer  to  CFD  results.
■590    ▼aSchool  code:  0176.
■650  4▼aAircraft
■650  4▼aVortices
■650  4▼aAcoustics
■650  4▼aReynolds  number
■650  4▼aGeometry
■650  4▼aRadiation
■650  4▼aAerodynamics
■650  4▼aAerospace  engineering
■650  4▼aFluid  mechanics
■690    ▼a0986
■690    ▼a0538
■690    ▼a0800
■690    ▼a0204
■71020▼aThe  Pennsylvania  State  University.
■7730  ▼tDissertations  Abstracts  International▼g87-04B.
■790    ▼a0176
■791    ▼aPh.D.
■792    ▼a2025
■793    ▼aEnglish
■85640▼uhttp://www.riss.kr/pdu/ddodLink.do?id=T17360194▼nKERIS▼z이  자료의  원문은  한국교육학술정보원에서  제공합니다.

미리보기

내보내기

chatGPT토론

Ai 추천 관련 도서


    신착도서 더보기
    최근 3년간 통계입니다.

    소장정보

    • 예약
    • 소재불명신고
    • 나의폴더
    • 우선정리요청
    • 비도서대출신청
    • 야간 도서대출신청
    소장자료
    등록번호 청구기호 소장처 대출가능여부 대출정보
    TF18901 전자도서 대출가능 마이폴더 부재도서신고 비도서대출신청 야간 도서대출신청

    * 대출중인 자료에 한하여 예약이 가능합니다. 예약을 원하시면 예약버튼을 클릭하십시오.

    해당 도서를 다른 이용자가 함께 대출한 도서

    관련 인기도서

    로그인 후 이용 가능합니다.