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Rocket-model Investigation of Longitudinal Stability and Drag Characteristics of an Airplane Configuration Have a 60° Delta Wing and a High Unwept Horizontal Tail

by Robert F. Peck, Jesse L. Mitchell

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Rocket-model Investigation of Longitudinal Stability and Drag Characteristics of an Airplane Configuration Have a 60° Delta Wing and a High Unwept Horizontal Tail

by Robert F. Peck, Jesse L. Mitchell

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Book Details

Publisher:: National Advisory Committee for Aeronautics
Published:: 1953
Pages:: 28
Language:: EN
ISBN:: Unknown