867 research outputs found
Low-speed static lateral stability characteristics of a canard model having a 60 degrees triangular wing and horizontal tail
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Collection and Analysis of Wind-tunnel Data on the Characteristics of Isolated Tail Surfaces with and Without End Plates
Get PDFLow-speed static longitudinal stability characteristics of a canard model having a 60 degrees triangular wing and horizontal tail
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Dynamic Stability and Control Characteristics of a Delta-wing Vertically Rising Airplane Model in Take-offs, Landings and Hovering Flight
Get PDFPreliminary Investigation at Low Speed of Downwash Characteristics of Small-scale Sweptback Wings
Get PDFAdditional Studies of the Stability and Controllability of an Unswept-wing Vertically Rising Airplane Model in Hovering Flight Including Studies of Various Tethered Landing Techniques
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NACA Research Memorandums
Get PDFContains the results of an investigation in the Langley free-flight tunnel to determine the stability and control characteristics of a 1/12-scale dynamic free-flying model of the Consolidated Vultee 7002 airplane (a flying mock-up of the XP-92 airplane). The wing and vertical tail of this model were of triangular plan form with 60 degree sweepback of the leading edge. The results of both force and flight tests of the model are presented
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