Adaptive Variable-Fidelity Analysis and Design of A Tailless Aircraft under Model-Form Uncertainty

Cited 9 time in webofscience Cited 0 time in scopus
  • Hit : 258
  • Download : 0
Publisher
AIAA Scitech 2016
Issue Date
2016-01-04
Language
English
Citation

AIAA Scitech 2016

URI
http://hdl.handle.net/10203/205964
Appears in Collection
AE-Conference Papers(학술회의논문)
Files in This Item
There are no files associated with this item.
This item is cited by other documents in WoS
⊙ Detail Information in WoSⓡ Click to see webofscience_button
⊙ Cited 9 items in WoS Click to see citing articles in records_button

qr_code

  • mendeley

    citeulike


rss_1.0 rss_2.0 atom_1.0