Feasibility study of a novel load alleviation system on the UH-60A Blackhawk helicopter

Title

Feasibility study of a novel load alleviation system on the UH-60A Blackhawk helicopter

Author

Verhagen, M.R.

Contributor

Voskuijl, M. (mentor)

Faculty

Aerospace Engineering

Department

Aerospace Design, Integration & Operations

Programme

Flight Performance and Propulsion

Date

2015-08-06

Subject

helicopter
structural load alleviation system
SLA
tailplane
horizontal stabilizer
Flightlab
UH-60A
Blackhawk
agility
safety
flightpath bandwidth

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http://resolver.tudelft.nl/uuid:b4b1fe9c-acb6-4e2b-adc6-5324dfbaf51c

Embargo date

2016-08-06

Part of collection

Student theses

Document type

master thesis

Rights

(c) 2015 Verhagen, M.R.