Robuts design of trailing edge flap with orthogonal array inspired response surface for helicopter vibration reduction

Thumbnail Image

Files

erf_2013_018.pdf (2.45 MB)

Date

2013

Authors

Journal Title

Journal ISSN

Volume Title

Publisher

Abstract

Description

Keywords

Citation

URI

http://hdl.handle.net/20.500.11881/588

Collections

Papers

Endorsement

Review

Supplemented By

Referenced By