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NASA NTRS · 19630000199

DESIGN CONCEPTS FOR MINIMUM WEIGHT, HIGH PERFORMANCE SUPERSONIC AIRCRAFT STRUCTURES

Abstract

Wing and fuselage concepts for supersonic aircraft

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BibTeXRIS

Dunning, J. S., Rowe, G. T.. 1962-10-01. DESIGN CONCEPTS FOR MINIMUM WEIGHT, HIGH PERFORMANCE SUPERSONIC AIRCRAFT STRUCTURES. https://ntrs.nasa.gov/citations/19630000199

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