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Tests of a Hermes A-2 Missile Body at Mach Number 4.04

An Investigation of Flow Characteristics at Mach Number 4.04 Over 6- and 9-Percent-Thick Symmetrical Circular-Arc Airfoils Having 30-Percent-Chord Trailing-Edge Flaps

Aerodynamic Characteristics of Two Delta Wings at Mach Number 4.04 and Correlations of Lift and Minimum-Drag Data for Delta Wings at Mach Numbers From 1.62 to 6.9

Aerodynamic Characteristics of Low-aspect-ratio Wings at High Supersonic Mach Numbers

Normal force, center of pressure, and zero-lift drag of several ballistic-type missiles at Mach numbers of 4.05

Longitudinal and lateral aerodynamic characteristics at combined angles of attack and sideslip of a generalized missile model having a rectangular wing at a Mach number of 4.08


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