A Technique for Shortening Landing Run Distance of an Aircraft by Symmetrical Deflection of Split Elevator and Rudder
Crossref DOI link: https://doi.org/10.3103/S106879981802006X
Published Online: 2019-01-19
Published Print: 2018-04
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Bazuhair, M. A.
Text and Data Mining valid from 2018-04-01
Article History
Received: 26 April 2017
First Online: 19 January 2019