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NACA-TR-522

The drag of airplane wheels, wheel fairings, and landing gears - III

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:41:01Z
date available2017-09-04T16:41:01Z
date copyright01/01/1936
date issued1936
identifier otherBRWUYDAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/104290
description abstractThe tests reported in this report conclude the investigation of landing-gear drag that has been carried out in the NACA 20-foot wind tunnel. They supplement earlier tests (reported in Technical Report No. 485) made with full-scale dummy wheels, wheel fairings, and landing gears intended for airplanes of 3,000 pounds gross weight and include tests of tail wheels and tail skids.
languageEnglish
titleNACA-TR-522num
titleThe drag of airplane wheels, wheel fairings, and landing gears - IIIen
typestandard
page11
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1936
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsBODIES
subject keywordsCANTILEVER
subject keywordsCOMPARISON
subject keywordsDRAG
subject keywordsFAIRINGS
subject keywordsGEAR
subject keywordsINTERFERENCE
subject keywordsLANDING
subject keywordsMEMBERS
subject keywordsSTREAMLINED
subject keywordsTESTS
subject keywordsTRIPODS
subject keywordsTUNNEL
subject keywordsWHEELS
subject keywordsWIND


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