Wind-tunnel investigation of the aerodynamic pressures on the Apollo launch escape vehicle configuration
Wind tunnel investigation of aerodynamic pressures on Apollo launch escape vehicle configuration
Engineering topics
Publications and source records attributed to Moseley, W. C., Jr..
Wind tunnel investigation of aerodynamic pressures on Apollo launch escape vehicle configuration
Wind tunnel study of aerodynamic pressures on Apollo command module configuration
Aerodynamic loads on deployed canard surfaces and rocket nose section of Apollo launch escape vehicle
Aerodynamic characteristics determined during development of Apollo launch escape vehicle configuration in wind tunnel tests
Wind tunnel test data on static and dynamic stability of Apollo command module configuration
Aerodynamic stability of Apollo launch escape vehicle
Wind tunnel tests of Apollo command module static and dynamic stability characteristics
Apollo wind tunnel test program and configuration design developments
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Hinge moment and flutter characteristics of flap- type controls - free oscillation tests of changes in control profile and control trailing- edge angle
Control trailing-edge thickness and aspect ratio effect on oscillating hinge-moment and flutter characteristics of flap-type controls
Free oscillation test to determine hinge moment of trailing-edge, flap control surface with various hinge-line positions at transonic speed