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1970•Unpublished venueRequires access

DAMPING-IN-PITCH DERIVATIVES OF 120- AND 140-DEG BLUNTED CONES AT MACH NUMBERS FROM 0.6 THROUGH 3

Bob L. Uselton, T. O. Shadow, A. C. Mansfield

Open publisher page 5 citations

Abstract

Approved for public release; distribution is unlimited. Document partially illegible. Distribution authorized to U.S. Gov't. agencies only; Administrative/Operational Use; APR 1970. Other requests shall be referred to National

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Approved for public release; distribution is unlimited. Document partially illegible. Distribution authorized to U.S. Gov't. agencies only; Administrative/Operational Use; APR 1970. Other requests shall be referred to National

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OpenAlex reports 5 citations for this work. Citation counts describe recorded attention and do not establish research quality.

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Available abstract

Approved for public release; distribution is unlimited. Document partially illegible. Distribution authorized to U.S. Gov't. agencies only; Administrative/Operational Use; APR 1970. Other requests shall be referred to National

Key concepts: Mach number, Reynolds number, Angle of attack, Physics, Mechanics, Wind tunnel, Oscillation (cell signaling), Mathematics

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DAMPING-IN-PITCH DERIVATIVES OF 120- AND 140-DEG BLUNTED CONES AT MACH NUMBERS FROM 0.6 THROUGH 3 — Research Paper | ScholarLens