NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Aeroelastic Model Tuning for Precise Flutter PredictionNo abstract available
Document ID
20160011961
Acquisition Source
Armstrong Flight Research Center
Document Type
Presentation
Authors
Pak, Chan-Gi (NASA Armstrong Flight Research Center Edwards, CA, United States)
Date Acquired
October 4, 2016
Publication Date
September 28, 2016
Subject Category
Research And Support Facilities (Air)
Avionics And Aircraft Instrumentation
Air Transportation And Safety
Report/Patent Number
DFRC-E-DAA-TN33432
Report Number: DFRC-E-DAA-TN33432
Meeting Information
Meeting: Mechanical Engineering Class
Location: Daejeon
Country: Korea, Republic of
Start Date: September 28, 2016
Sponsors: Gwangju Inst. of Science and Technology
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
aerodynamic load sensing
fiber optic strain sensor
shape sensing

Related Records

There are no records associated with this record.
No Preview Available