Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
experimental aircraft technology
|
| gptkbp:aircraftTested |
gptkb:F/A-18A_(No._853)
|
| gptkbp:demonstrates |
potential for lighter wings
active control of wing flexibility aeroelastic tailoring improved roll performance |
| gptkbp:developedBy |
gptkb:NASA
gptkb:U.S._Air_Force |
| gptkbp:firstFlight |
November 2002
|
| gptkbp:fundedBy |
gptkb:Air_Force_Research_Laboratory
gptkb:Boeing_Phantom_Works gptkb:NASA_Dryden_Flight_Research_Center |
| gptkbp:goal |
reduce weight and complexity of aircraft control systems
|
| https://www.w3.org/2000/01/rdf-schema#label |
Active Aeroelastic Wing
|
| gptkbp:purpose |
to demonstrate control of aircraft using wing flexibility
|
| gptkbp:relatedTo |
gptkb:X-53_Active_Aeroelastic_Wing
|
| gptkbp:startYear |
1996
2005 |
| gptkbp:technology |
aeroelastic control
|
| gptkbp:testedBy |
F/A-18 Hornet
|
| gptkbp:testLocation |
gptkb:NASA_Dryden_Flight_Research_Center
|
| gptkbp:uses |
wing twist for roll control
|
| gptkbp:bfsParent |
gptkb:Convair_X-53
|
| gptkbp:bfsLayer |
6
|