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
Moseley, W. C., Jr.↗
Engineering topics
Moseley, W. C., Jr.
Publications and source records attributed to Moseley, W. C., Jr..
Wind-tunnel investigation of the aerodynamic pressures on the Apollo command module configuration
Wind tunnel study of aerodynamic pressures on Apollo command module configuration
Moseley, W. C., Jr.↗
Aerodynamic loads on deployed canard surfaces and rocket nose section of the Apollo launch escape vehicle
Aerodynamic loads on deployed canard surfaces and rocket nose section of Apollo launch escape vehicle
Moseley, W. C., Jr.↗
Aerodynamic characteristics determined during development of the Apollo launch escape vehicle configuration
Aerodynamic characteristics determined during development of Apollo launch escape vehicle configuration in wind tunnel tests
Bowen, F. E.↗
Aerodynamic stability characteristics of the Apollo command module
Wind tunnel test data on static and dynamic stability of Apollo command module configuration
Graham, R. E.↗
Aerodynamic stability characteristics of the Apollo launch escape vehicle
Aerodynamic stability of Apollo launch escape vehicle
LAUNCH ESCAPE SYSTEM /LES/↗
Stability Characteristics of the Apollo Command Module
Wind tunnel tests of Apollo command module static and dynamic stability characteristics
STATIC STABILITY↗
Apollo wind tunnel testing program - Historical development of general configurations
Apollo wind tunnel test program and configuration design developments
SPACECRAFT DESIGN↗
Summary of wind-tunnel investigations of the static longitudinal stability characteristics of the production Mercury configurations at Mach numbers from 0.05 to 20
Explore the source record for details and available documents.
Brown, S. W.↗
Some effects of control profile and control trailing-edge angle on the oscillating hinge-moment and flutter characteristics of flap-type controls at transonic speeds
Hinge moment and flutter characteristics of flap- type controls - free oscillation tests of changes in control profile and control trailing- edge angle
FLUTTER↗
EFFECT OF CONTROL TRAILING-EDGE THICKNESS OR ASPECT RATIO ON THE OSCILLATING HINGE-MOMENT AND FLUTTER CHARACTERISTICS OF A FLAPTYPE CONTROL AT TRANSONIC SPEEDS
Control trailing-edge thickness and aspect ratio effect on oscillating hinge-moment and flutter characteristics of flap-type controls
DAMPING↗
EFFECT OF HINGE-LINE POSITION ON THE OSCILLATING HINGE MOMENTS AND FLUTTER CHARACTERISTICS OF A FLAP-TYPE CONTROL AT TRANSONIC SPEEDS
Free oscillation test to determine hinge moment of trailing-edge, flap control surface with various hinge-line positions at transonic speed
FLUTTER↗