Publication Date:
2019-07-11
Description:
Force tests on a proposed body shape of the Hermes A-2 missile with and without longitudinal spoilers were made at Mach number 4.04. Values of normal force coefficient, pitching-moment coefficient, and center-of-pressure position were obtained.
Keywords:
Aerodynamics
Type:
NACA-RM-SL50H23A
Format:
application/pdf