Output details
15 - General Engineering
University of Glasgow
Return to search
Output 0 of 0 in the submission
Article title
Calculation of rotorcraft inflow coefficients using blade flapping measurements
Type
D - Journal article
DOI
Title of journal
Journal of Aircraft
Article number
-
Volume number
46
Issue number
5
First page of article
1569
ISSN of journal
0021-8669
Year of publication
2009
URL
-
Number of additional authors
1
Additional information
Data gathered during UK Civil Aviation Authority funded flight testing (CAA Contract 7D/S/1125) in support of efforts to update the British Civil Airworthiness Requirements (BCAR) Section T (www.caa.co.uk/docs/33/Paper2009_02red.pdf) were used to validate rotor-induced velocity models using an implicit method. The paper describes a framework for applying finite state wake models to rotorcraft in general, with the results validated against actual flight data. The results of this work were unique as they included blade flapping measurements, and the tests were all in autorotative flight.
Interdisciplinary
-
Cross-referral requested
-
Research group
D - Aerospace Sciences
Proposed double-weighted
No
Double-weighted statement
-
Reserve for a double-weighted output
No
Non-English
No
English abstract
-
