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Language: en
Pages: 58

Experimental Study at Low Supersonic Speeds of a Missile Concept Having Opposing Wraparound Tails

Authors: National Aeronautics and Space Administration (NASA)

Categories:

Type: BOOK - Published: 2018-07-06 - Publisher: Createspace Independent Publishing Platform

A wind-tunnel investigation has been performed at low supersonic speeds (at Mach numbers of 1.60, and 2.16) to evaluate the aerodynamic characteristics of a mis

Language: en
Pages: 64

Experimental Study at Low Supersonic Speeds of a Missile Concept Having Opposing Wraparound Tails

Authors: Jerry M. Allen

Categories: Fins (Anatomy)

Type: BOOK - Published: 1994 - Publisher:

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Abstract: A wind-tunnel investigation has been performed at low supersonic speeds (at Mach numbers of 1.60, 1.90, and 2.16) to evaluate the aerodynamic characte