Add to ORKGNumerical solution of combined hydrodynamic and shell equations for hydroelastic response of flexible shell
Application of analysis and models to structural dynamic problems related to Apollo-Saturn 5 launch ...
Nonlinear structural analysis of stress and buckling pressures of aft heat shield of Apollo spacecra...
Hydrodynamic impact tests were made on an elastic model approximating a two-mass spring system to de...
Mathematical model for predicting dynamic response of thin elastic shells of revolution during water...
Computer program for hydroelastic responses of flexible shells of revolution during axially symmetri...
Analysis of linear elastic thin shells of revolution subjected to arbitrary temperatures and loads -...
Comparison of theoretical Apollo water impact data with scale model experimental result
Apollo spacecraft landing simulation to determine impact water pressures, accelerations, and landing...
Structural analysis of Apollo aft heat shield under water impact loading condition
Hydrodynamic impact simulated by impacting rigid, right circular cylinder on smooth water surface, a...
Effect of heat shield flexibility on water landing loads of Apollo spacecraft model
Impact water pressures, accelerations, and landing dynamics of scale model Apollo command module wit...
FORTRAN 5 digital computer program for predicting dynamic response of Apollo command module to earth...
An experimental investigation was made to determine impact water pressures, accelerations, and landi...
The hydrodynamic impact of a falling body upon a viscous incompressible fluid was investigated by nu...
Application of analysis and models to structural dynamic problems related to Apollo-Saturn 5 launch ...
Nonlinear structural analysis of stress and buckling pressures of aft heat shield of Apollo spacecra...
Hydrodynamic impact tests were made on an elastic model approximating a two-mass spring system to de...
Mathematical model for predicting dynamic response of thin elastic shells of revolution during water...
Computer program for hydroelastic responses of flexible shells of revolution during axially symmetri...
Analysis of linear elastic thin shells of revolution subjected to arbitrary temperatures and loads -...
Comparison of theoretical Apollo water impact data with scale model experimental result
Apollo spacecraft landing simulation to determine impact water pressures, accelerations, and landing...
Structural analysis of Apollo aft heat shield under water impact loading condition
Hydrodynamic impact simulated by impacting rigid, right circular cylinder on smooth water surface, a...
Effect of heat shield flexibility on water landing loads of Apollo spacecraft model
Impact water pressures, accelerations, and landing dynamics of scale model Apollo command module wit...
FORTRAN 5 digital computer program for predicting dynamic response of Apollo command module to earth...
An experimental investigation was made to determine impact water pressures, accelerations, and landi...
The hydrodynamic impact of a falling body upon a viscous incompressible fluid was investigated by nu...
Application of analysis and models to structural dynamic problems related to Apollo-Saturn 5 launch ...
Nonlinear structural analysis of stress and buckling pressures of aft heat shield of Apollo spacecra...
Hydrodynamic impact tests were made on an elastic model approximating a two-mass spring system to de...