The upper wing surfaces of the Active Aeroelastic Wing F/A-18 test aircraft are covered with accelerometers and other sensors during ground vibration tests at NASA Dryden Flight Research Center. EC02-0203-46
Summary
The upper wing surfaces of the Active Aeroelastic Wing F/A-18 test aircraft are covered with accelerometers and other sensors during ground vibration tests at NASA Dryden Flight Research Center.
- X-53 (F/A-18A TN 853 Active Aeroelastic Wing [AAW]) - NASA
- X-53 (F/A-18A TN 853 Active Aeroelastic Wing [AAW]) NASA
- X-53 (F/A-18A TN 853 Active Aeroelastic Wing [AAW]) NASA
- X-53 (F/A-18A TN 853 Active Aeroelastic Wing [AAW]) NASA
- X-53 (F/A-18A TN 853 Active Aeroelastic Wing [AAW]) NASA
- X-53 (F/A-18A TN 853 Active Aeroelastic Wing [AAW]) NASA
- Boeing X-53 Active Aeroelastic Wing Wikiwand, 54% OFF
- X-53 Active Aeroelastic Wing (F/A-18 AAW), 55% OFF
- X-53 (F/A-18A TN 853 Active Aeroelastic Wing [AAW]) NASA
- Soubor:FA-18 Active Aeroelastic Wing (AAW) on – Wikipedie
Tags
active aeroelastic wing
aaw
f a 18
f 18
ground vibration testing
afrc
nasa tom tschida
armstrong flight research center
surfaces
active
aeroelastic
active aeroelastic
aircraft
test aircraft
accelerometers
sensors
ground
vibration
ground vibration tests
dryden
flight
research
center
nasa dryden flight research center
test flight
high resolution
experimental aircraft
nasa
dryden flight research center
california
Date
22/08/2002
Location
Armstrong Flight Research Center
,
34.95855, -117.89067
Source
NASA
Link
Copyright info
Public Domain Dedication (CC0)