A computer code is developed to generate plots using UNIVAC 1100 system and CALCOMP 1039 plotter. The plots give spanwise load distribution on wings

Sridharan, R

Viswanathan, S

English

National Aerospace Laboratories Institutional Repository

1 . Security Classification of this Page-----------------------------------------------------------------------2 . Type of DocumentProject Document------------------------------- ----------------------------------------3 . Report No .	: 4 . Date 5 . Security Classification/Declassification SchedulePD AN 8527 : Nov.1985---------------------------------------------------------------- -------6 . Title/Sub-titleA Computer Code for Generating Plots of LoadDistribution on Spanwise Sections on a wing-----------------------------------------------------------------------7 . Author(s)R .Sridharan, S.Viswanathan-----------------------------------------------------------------------8 . Division/SectionAerodyn,9 . Project No .AR-610-----------------------------------------------------------------------10 .Type of report/ : 11 . pages [ 5] : 12 . Approved by/Period covered tables [ 1] : No.of copiesillustrations [Project Document19]' 4^tip".' ~~ s	Head,Aerodyn,Divei./15 Copse13 .a) Sponsoring Agency(s) 13 .o) rarticipating Agency(s)------------------------------------------------------------------------14 .Keywords !Computer code, Calcomp plotter, Load distribution, 1Spanwise sections on wing-------------------------------------------------------------15 . AbstractA computer code is developed to generate plotsusing UNIVAC 1100 system and CALCOMP 1039 plotter, Theplots give spanwise load distribution on wings .1171------------------------------------------------------------------------NATIONAL AERONAUTICAL LABORATORYBANGALORE, INDIA

A Computer Code for Generating Plots of Load

Distribution on Spanwise Sections on a wing

NAL-IR

A Computer Code for Generating Plots of Load\ud
Distribution on Spanwise Sections on a wing

http://nal-ir.nal.res.in/11031/1/PD_AE_8527.pdf

A Computer Code for Generating Plots of Load Distribution on Spanwise Sections on a wing

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