A THEORETICAL INVESTIGATION OF THE EFFECTS OF THE CONFIGURATIVE DESIGN OF A SPACE VEHICLE ON ITS STRUCTURAL BENDING FREQUENCIES AND AERODYNAMIC STABILITY
Space vehicle configuration effects on structural bending frequencies and aerodynamic stability
SEARCH · Search NASA
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Space vehicle configuration effects on structural bending frequencies and aerodynamic stability
Resonant bending frequencies and mode shapes for thin circular cylindrical shell containing an internal liquid with a free surface
Forces and moments of liquid propellant oscillation in cylindrical tanks caused by structural bending
Control techniques for the solution of structural bending and elastic feedback of flexible boosters
Resonant bending frequencies and mode shapes for thin, circular cylindrical shell containing an internal liquid with a free surface
Bending vibration of circular cylindrical shell with internal liquid having free surface
Flight evaluation of vehicle bending data for saturn i launch vehicle - structural vibration, dynamic response
Cumulative rotating bending fatigue damage in steels and in an aluminum alloy
Effect of crystal orientation on slip surface and dislocation structures of beryllium in bending fatigue
Oscilloscope display of space vehicle bending motions using switching circuit for sampling accelerometer outputs from vehicle
Collapse tests of pressurized membrane-like circular cylinders subjected to compression loading and bending moment
Bending test for measuring ductility of refractory metal alloy weldments
Fluid flow velocity effects on frequency of bending vibrations of simply supported pipe
Metal rectangular plate bending analysis with nonlinear strain hardening, creep yielding stress and deflection expressions as functions of position and time
Matrix-Holzer method for predicting free vibration modes of clustered launch vehicles in bending applied to first eight modes of Saturn I model
Stress-intensity factors for three-point bending by boundary value collocation - structural dynamics
Buckling test of truss-core sandwich cylinder loaded in bending - cylinder failure due to growth of wall buckles
Large diameter ring stiffened corrugated cylinder bending tests