Numerical lifting line theory applied to drooped leading-edge wings below and above stall /

19

Bibliographic Details
Main Authors: 188452 Anderson, John David, Corda, Stephen, Van Wie, David M.
Format:
Subjects:
_version_ 1796723228812509184
author 188452 Anderson, John David
Corda, Stephen
Van Wie, David M.
author_facet 188452 Anderson, John David
Corda, Stephen
Van Wie, David M.
author_sort 188452 Anderson, John David
collection OCEAN
description 19
first_indexed 2024-03-05T07:27:23Z
format
id KOHA-OAI-TEST:379191
institution Universiti Teknologi Malaysia - OCEAN
last_indexed 2024-03-05T07:27:23Z
record_format dspace
spelling KOHA-OAI-TEST:3791912020-12-19T17:13:13ZNumerical lifting line theory applied to drooped leading-edge wings below and above stall / 188452 Anderson, John David Corda, Stephen Van Wie, David M. 19PSZJBLLift (Aerodynamics)
spellingShingle Lift (Aerodynamics)
188452 Anderson, John David
Corda, Stephen
Van Wie, David M.
Numerical lifting line theory applied to drooped leading-edge wings below and above stall /
title Numerical lifting line theory applied to drooped leading-edge wings below and above stall /
title_full Numerical lifting line theory applied to drooped leading-edge wings below and above stall /
title_fullStr Numerical lifting line theory applied to drooped leading-edge wings below and above stall /
title_full_unstemmed Numerical lifting line theory applied to drooped leading-edge wings below and above stall /
title_short Numerical lifting line theory applied to drooped leading-edge wings below and above stall /
title_sort numerical lifting line theory applied to drooped leading edge wings below and above stall
topic Lift (Aerodynamics)
work_keys_str_mv AT 188452andersonjohndavid numericalliftinglinetheoryappliedtodroopedleadingedgewingsbelowandabovestall
AT cordastephen numericalliftinglinetheoryappliedtodroopedleadingedgewingsbelowandabovestall
AT vanwiedavidm numericalliftinglinetheoryappliedtodroopedleadingedgewingsbelowandabovestall