| Nalla 1 : Data report-Part I (1991) | |||||||||||||
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| National Aeronautical Laboratory lillllllllllllllllllllllllll Nalla Data Report Part ASHOK KARTHIK SATHISH SATISH ROHIDEKAR Flight Experiments Division Project Document M September Bangalore India oft NAP AVAW ABSTRACT This report gives the leading geometric particulars well the center cavity anc moment iiier tiA NALLA corifi uvaLion a NOTE The dat on July extracted from aster data files maintained the NALLA design office These filee continuously updated and should refer for latest information However fresh report will issued when the number chari become niIic unt CONTENTS DESIGN FEATURES DESIGN PRIORITIES SPECIAL FEATURES SPECIFICATIONS GEOMETRIC DETAILS BASIC DIMENSIONS COMPUTED DIMENSIONS WEIGHT AND MOMENTS INERTIA ESTIMATES ESTIMATES WEIGHT AND MOMENT INERTIA BREAKDOWN ACKNOWLEDGMENTS APPENDIX LI z Ul m J CD cd f L J LLJ n DESIGN FEATURES DESIGN PRIORITIES Low aircraft acquisition cost Low aircraft operation cost iii Ruggedness for flying training Good low speed handling Simple maintenance features Reasonable cross country flight capabilities vii Acrobatic capabilities for future SPECIAL FEATURES Pusher propeller Laminar flow aerofoils iii Carbon and glass fibre reinforced plastics construction Tricycle landing gear Proven engine Simple control systems SPECIFICATIONS NALLA Two seat light aircraft mainly for initio flying training low wing pusher propeller Fig Semi acrobatic Category Side side with dual controls Seating Landing gear Tricycle Wing span Wing area All Weight | |||||||||||||
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