Water tunnel flow visualization studies of a Canard-Configured X-31A- like fighter aircraft model
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Authors
Kwon, Hui Man
Subjects
Effect of canard location
pitch and pitch rate
vortex development and bursting
flow visualization by dye injection
water tunnel studies
X-31-like fighter aircraft model
Engineering
Aeronautics
pitch and pitch rate
vortex development and bursting
flow visualization by dye injection
water tunnel studies
X-31-like fighter aircraft model
Engineering
Aeronautics
Advisors
Hebbar, S.K.
Platzer, M.F.
Date of Issue
Date
1990
Publisher
Monterey, California. Naval Postgraduate School
Language
en_US
Abstract
Type
Thesis
Description
Series/Report No
Department
Aeronautics and Astronautics
Organization
Naval Postgraduate School (U.S.)
Identifiers
NPS Report Number
Sponsors
Funder
Format
vi, 111 p.: ill.
Citation
Distribution Statement
Approved for public release; distribution is unlimited.
Rights
Copyright is reserved by the copryright owner.