SwePub
Sök i LIBRIS databas

  Utökad sökning

WFRF:(Mårtensson Stefan)
 

Sökning: WFRF:(Mårtensson Stefan) > Aeroelastic propert...

Aeroelastic properties of closely spaced modes for a highly loaded transonic fan

Mårtensson, H. (författare)
Gunnsteinsson, Stefan Sturla (författare)
KTH,Kraft- och värmeteknologi
Vogt, Damian M. (författare)
KTH,Kraft- och värmeteknologi
 (creator_code:org_t)
2008
2008
Engelska.
Serie: Proceedings of the ASME Turbo Expo ; 5
  • Konferensbidrag (refereegranskat)
Abstract Ämnesord
Stäng  
  • In the design of modem compressor blades of wide chord (low aspect ratio) type it is often hard to avoid having modes that are close to each other in frequency. Modes which are closely spaced can interact dynamically. Mistuning and localization of stresses are known problems with this. A potential problem with this is also the possibility of coalescence flutter of the modes. Even if the modes are frequency separated at zero rotational speed, the centrifugal stiffening may cause the modes to attract and even cross (or veer) at some rotational speed. In design, mode separation criteria are sometimes applied in order to minimize the risk of encountering unknown dynamic phenomena. This study is performed to better understand the dynamics of closely spaced modes with respect to risk for coalescence flutter. A reduced order aeroelastic system is then constructed that describes the interaction between the different modes. The aeroelastic couplings are then calculated for the 2 mode system. The method is general in terms of mode shapes and number of interacting modes. A parametrical study is performed in order to study how strongly the modes interact when the frequency separation is decreased and if there is a risk of destructive coalescence flutter. The investigation is performed on a high pressure ratio front stage fan blade. The tendency of the modes to interact depends on the strength of the coupling compared to the strength of the pure structural modes. The tendency towards instability was increased in cases where the stability margin was smaller of the single modes. The results can be considered to support a separation criterion of 2% for the lower. A re-evaluation should be considered if lighter blade material and increased loads are to be used.

Ämnesord

TEKNIK OCH TEKNOLOGIER  -- Maskinteknik -- Rymd- och flygteknik (hsv//swe)
ENGINEERING AND TECHNOLOGY  -- Mechanical Engineering -- Aerospace Engineering (hsv//eng)

Nyckelord

Aeroelastic coupling
Aeroelastic properties
Aeroelastic system
Centrifugal stiffening
Compressor blades
Different modes
Dynamic phenomena
Fan blades
Frequency separation
High pressure ratio
Low aspect ratio
Mistuning
Mode separation
Mode shapes
Potential problems
Re-evaluation
Reduced order
Rotational speed
Separation criterion
Single mode
Stability margins
Structural modes
Aspect ratio
Centrifugation
Flutter (aerodynamics)
Coalescence

Publikations- och innehållstyp

ref (ämneskategori)
kon (ämneskategori)

Till lärosätets databas

Hitta mer i SwePub

Av författaren/redakt...
Mårtensson, H.
Gunnsteinsson, S ...
Vogt, Damian M.
Om ämnet
TEKNIK OCH TEKNOLOGIER
TEKNIK OCH TEKNO ...
och Maskinteknik
och Rymd och flygtek ...
Delar i serien
Av lärosätet
Kungliga Tekniska Högskolan

Sök utanför SwePub

Kungliga biblioteket hanterar dina personuppgifter i enlighet med EU:s dataskyddsförordning (2018), GDPR. Läs mer om hur det funkar här.
Så här hanterar KB dina uppgifter vid användning av denna tjänst.

 
pil uppåt Stäng

Kopiera och spara länken för att återkomma till aktuell vy