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Wind-tunnel investigation of effect of interference on lateral-stability characteristics of four NACA 23012 wings, an elliptical and a circular fuselage and vertical fins

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:41:18Z
date available2017-09-04T18:41:18Z
date copyright01/01/1941
date issued1941
identifier otherJWWUYDAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;jsessionid=3826AF679D40527318548F1EFDEC014A/handle/yse/222888
description abstractReport presents the results of a wind-tunnel investigation of the effect of wing-fuselage interference on lateral-stability characteristics made in the NACA 7 by 10-foot wind tunnel on four fuselages and two fins, representing high-wing, low-wing, and midwing monoplanes. The fuselages are of circular and elliptical cross section. The wings have rounded tips and, in plan form, one is rectangular and the three are tapered 3:1 with various amounts of sweep. The rate of change in the coefficients of rolling moment, yawing moment, and lateral force with angle of yaw is given in a form to show the increment caused by wing-fuselage interference for the model with no fin and the effect of wing-fuselage interference on fin effectiveness. Results for the fuselage-fin combination and the wing tested alone are also given.
languageEnglish
titleNACA-TR-705num
titleWind-tunnel investigation of effect of interference on lateral-stability characteristics of four NACA 23012 wings, an elliptical and a circular fuselage and vertical finsen
typestandard
page20
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1941
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsAIRCRAFT
subject keywordsBODY
subject keywordsCIRCULAR
subject keywordsCONFIGURATIONS
subject keywordsELLIPTICITY
subject keywordsFUSELAGES
subject keywordsINTERFERENCE
subject keywordsLATERAL
subject keywordsMONOPLANES
subject keywordsPROFILES
subject keywordsSHELLS
subject keywordsSTABILITY
subject keywordsTESTS
subject keywordsTUNNEL
subject keywordsWIND
subject keywordsWING
subject keywordsWINGS


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