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Investigation of a 1/4-scale model of the Republic F-105 airplane in the Langley 19-foot pressure tunnel. Lateral control and directional stability and control characteristics of model equipped with drooped, supersonic-type, elliptical wing-root inlet

P. A. Canoro, H. N. Kelly

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Abstract

Defcrceof the Wmtcltid Shtes xithb t?z mi-luw of or li * rc1ePhm oi its ccJttcP.tsIn lo;' m,vLcr to -A uL~lltt3nZCzi clrs,n 1s pr0hlbltc~ by !m.

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Defcrceof the Wmtcltid Shtes xithb t?z mi-luw of or li * rc1ePhm oi its ccJttcP.tsIn lo;' m,vLcr to -A uL~lltt3nZCzi clrs,n 1s pr0hlbltc~ by !m.

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Available abstract

Defcrceof the Wmtcltid Shtes xithb t?z mi-luw of or li * rc1ePhm oi its ccJttcP.tsIn lo;' m,vLcr to -A uL~lltt3nZCzi clrs,n 1s pr0hlbltc~ by !m.

Key concepts: Airplane, Aileron, Scale (ratio), Stability (learning theory), Wing, Engineering, Structural engineering, Computer science

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Investigation of a 1/4-scale model of the Republic F-105 airplane in the Langley 19-foot pressure tunnel. Lateral control and directional stability and control characteristics of model equipped with drooped, supersonic-type, elliptical wing-root inlet — Research Paper | ScholarLens