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WIND-TUNNEL INVESTIGATION OF THE STATIC STABILITY OF A 1 56-SCALE MODEL OF THE X-1E AIRPLANE AT MACH NUMBERS OF 2.37, 2.98, AND 4.01

FRED M. SMITH

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Abstract

An investigation has been conducted in the Langley high Math number jet at Mach numbers of 2.37, 2.98, and 4.01 to determine the static stapresent wind-tunnel tests is reasonably indicative of flight data if flexibility effects of the full-scale vertical tail are considered.

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An investigation has been conducted in the Langley high Math number jet at Mach numbers of 2.37, 2.98, and 4.01 to determine the static stapresent wind-tunnel tests is reasonably indicative of flight data if flexibility effects of the full-scale vertical tail are considered.

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Available abstract

An investigation has been conducted in the Langley high Math number jet at Mach numbers of 2.37, 2.98, and 4.01 to determine the static stapresent wind-tunnel tests is reasonably indicative of flight data if flexibility effects of the full-scale vertical tail are considered.

Key concepts: Airplane, Mach number, Wind tunnel, Stability (learning theory), Longitudinal static stability, Scale (ratio), Scale model, Aerospace engineering

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WIND-TUNNEL INVESTIGATION OF THE STATIC STABILITY OF A 1 56-SCALE MODEL OF THE X-1E AIRPLANE AT MACH NUMBERS OF 2.37, 2.98, AND 4.01 — Research Paper | ScholarLens