Stability and control assessment of a blended-wing body airliner configuration

D Jung, MH Lowenberg

Research output: Chapter in Book/Report/Conference proceedingConference Contribution (Conference Proceeding)

14 Citations (Scopus)
Translated title of the contributionStability and control assessment of a blended-wing body airliner configuration
Original languageEnglish
Title of host publicationAIAA Atmospheric Flight Mechanics Conference, San Francisco, USA
Pages913 - 931
Number of pages29
Publication statusPublished - Aug 2005

Bibliographical note

Other identifier: AIAA-2005-6213

Cite this