Gaonkar, Gopal H and Nagaraja, CS and Nagabhushanam, J (1989) Prediction of inplane damping from deterministic and stochastic models. In: Vertica, 13 (2). pp. 143-158.
Full text not available from this repository. (Request a copy)Abstract
This paper reviews computational reliability, computer algebra, stochastic stability and rotating frame turbulence (RFT) in the context of predicting the blade inplane mode stability, a mode which is at best weakly damped. Computational reliability can be built into routine Floquet analysis involving trim analysis and eigenanalysis, and a highly portable special purpose processor restricted to rotorcraft dynamics analysis is found to be more economical than a multipurpose processor. While the RFT effects are dominant in turbulence modeling, the finding that turbulence stabilizes the inplane mode is based on the assumption that turbulence is white noise.
| Item Type: | Journal Article |
|---|---|
| Publication: | Vertica |
| Publisher: | Pergamon Elsevier Science Ltd |
| Additional Information: | Copyright of this article belongs to Pergamon Elsevier Science Ltd. |
| Department/Centre: | Division of Mechanical Sciences > Aerospace Engineering(Formerly Aeronautical Engineering) |
| Date Deposited: | 09 Aug 2010 06:35 |
| Last Modified: | 10 Aug 2010 06:13 |
| URI: | http://eprints.iisc.ac.in/id/eprint/31178 |
Actions (login required)
 |
View Item |
