Add to ORKGComparison of theoretical Apollo water impact data with scale model experimental result
Ablation and temperature data for Apollo heat shield material using Pacemaker vehicle for flight tes
Program predicts expected deformations and stresses in nonlinear simple geometric structures subject...
Nonlinear structural analysis of stress and buckling pressures of aft heat shield of Apollo spacecra...
Analysis of linear elastic thin shells of revolution subjected to arbitrary temperatures and loads -...
Impact water pressures, accelerations, and landing dynamics of scale model Apollo command module wit...
Computer program for hydroelastic responses of flexible shells of revolution during axially symmetri...
Numerical solution of combined hydrodynamic and shell equations for hydroelastic response of flexibl...
Movement of forward heat shield in Apollo command module turbulent reverse flow wak
Advanced manned spacecraft heat shield thermal strain analysis - equilibrium and stress equations, s...
Mathematical model for predicting dynamic response of thin elastic shells of revolution during water...
Launch vehicle flight tests of effects of Apollo heat shield irregularities on ablative material per...
Effect of heat shield flexibility on water landing loads of Apollo spacecraft model
Stiffness matrix solution for shells of revolution possessing variable thickness heat protectio
Large space structures are capable of large thermal deformations in the space environment. A case of...
Comparison of theoretical Apollo water impact data with scale model experimental result
Ablation and temperature data for Apollo heat shield material using Pacemaker vehicle for flight tes
Program predicts expected deformations and stresses in nonlinear simple geometric structures subject...
Nonlinear structural analysis of stress and buckling pressures of aft heat shield of Apollo spacecra...
Analysis of linear elastic thin shells of revolution subjected to arbitrary temperatures and loads -...
Impact water pressures, accelerations, and landing dynamics of scale model Apollo command module wit...
Computer program for hydroelastic responses of flexible shells of revolution during axially symmetri...
Numerical solution of combined hydrodynamic and shell equations for hydroelastic response of flexibl...
Movement of forward heat shield in Apollo command module turbulent reverse flow wak
Advanced manned spacecraft heat shield thermal strain analysis - equilibrium and stress equations, s...
Mathematical model for predicting dynamic response of thin elastic shells of revolution during water...
Launch vehicle flight tests of effects of Apollo heat shield irregularities on ablative material per...
Effect of heat shield flexibility on water landing loads of Apollo spacecraft model
Stiffness matrix solution for shells of revolution possessing variable thickness heat protectio
Large space structures are capable of large thermal deformations in the space environment. A case of...
Comparison of theoretical Apollo water impact data with scale model experimental result
Ablation and temperature data for Apollo heat shield material using Pacemaker vehicle for flight tes
Program predicts expected deformations and stresses in nonlinear simple geometric structures subject...