Alleviation of Vortex-Induced Asymmetric Loads

Abstract

Covers advancements in spacecraft and tactical and strategic missile systems, including subsystem design and application, mission design and analysis, materials and structures, developments in space sciences, space processing and manufacturing, space operations, and applications of space technologies to other fields.

References

Page 1

	Year	Citations
The effects of wake splitter plates on bluff-body flow in the range 10<sup>4</sup> < <i>R</i> < 5 × 10<sup>4</sup>. Part 2 C. J. Apelt, G. S. West Journal of Fluid Mechanics Unsteady FlowPart 1EngineeringSplitter PlatesWake Splitter Plates	1975	208
Pressure and force distributions on a sharp-nosed circular cylinder at large angles of inclination to a uniform subsonic stream P. J. Lamont, B. L. Hunt Journal of Fluid Mechanics AeroacousticsFlow ControlEngineeringFluid MechanicsBoundary Layer	1976	135
Onset of aerodynamic side forces at zero sideslip on symmetric forebodies at high angles of attack E. R. Keener, G. T. Chapman Mechanics and Control of Flight Conference EngineeringFluid MechanicsWind EngineeringBoundary LayerExtensive Wind-tunnel Tests	1974	107
Aeroelastic instability caused by slender payloads. Lars E. Ericsson Journal of Spacecraft and Rockets MissileSpace VehicleEngineeringMechanical EngineeringMissile Defense	1967	84
Characteristics of flow over inclined bodies of revolution H. Julian Allen, Edward W Perkins University of North Texas Digital Library (University of North Texas)	1951	83
Side forces on a tangent ogive forebody with a fineness ratio of 3.5 at high angles of attack and Mach numbers from 0.1 to 0.7 E. R. Keener, G. T. Chapman, L. M. Cohen, NASA Technical Reports Server (NASA) AeroacousticsEngineeringFluid MechanicsMechanical EngineeringMach Numbers	1977	68
Side-Force Alleviation on Slender, Pointed Forebodies at High Angles of Attack Dhanvada M. Rao Journal of Aircraft AeroacousticsAeronauticsKinesiologyEngineeringNew Device	1979	60
Asymmetric lateral-directional characteristics of pointed bodies of revolution at high angles of attack P. L. Coe, J. R. Chambers, William Letko NASA Technical Reports Server (NASA) AeroacousticsEngineeringPointed BodiesFluid MechanicsAsymmetric Moments	1972	52
Effects of Mach number and afterbody length on aerodynamic side forces at zero sideslip on symmetric bodies at high angles of attack E. R. Keener, G. T. Chapman, Robert L. Kruse 14th Aerospace Sciences Meeting Symmetric BodiesAeronauticsEngineeringAerodynamic Side ForcesAerospace Engineering	1976	48
A Study of the Effects of Body Shape on the Vortex Wakes of Inclined Bodies at a Mach Number of 2 Forrest E Gowen, Edward W Perkins University of North Texas Digital Library (University of North Texas) EngineeringFluid MechanicsMechanical EngineeringVortex WakesUnsteady Flow	1953	22

Page 1