Add to ORKGMinimization of total heat input for manned vehicles entering atmosphere at hyperbolic speed
A differential evolutionary algorithm has been executed to optimize the hypersonic aerodynamic and s...
A spacecraft designed to operate in a planetary atmosphere must have an adequate heat shield to with...
The recent resurgence of interest in blunt-body atmospheric entry for applications such as aeroassis...
Stagnation point radiative heating rates for manned vehicles entering the earth's atmosphere at para...
Aerodynamic heating of conical vehicles entering earth atmosphere at speeds greater than earth parab...
Long-range hypervelocity vehicles are studied in terms of their motion in powered flight, and their ...
A simplified analysis of the velocity and deceleration history of missiles entering the earth's atmo...
An analysis has been made of atmosphere entries for which the vehicle lift-drag ratio was modulated ...
The results of an analysis of the motion and heating during atmospheric reentry of manned space vehi...
An extensive, low-perigee orbital aerodynamic heating study was undertaken in support of the Atmosph...
This is a study of performance and control for transatmospheric (TAV) aerospace planes, that use ai...
A general method has been developed, using the methods of kinetic theory, whereby the surface temper...
Laboratory simulation of hypervelocity heat transfer problem during planetary entr
The dimensionless, transformed, nonlinear differential equation developed in NASA TR R-11 for descri...
The ballistic vehicle is found to be the least efficient of the several types studied in the sense t...
A differential evolutionary algorithm has been executed to optimize the hypersonic aerodynamic and s...
A spacecraft designed to operate in a planetary atmosphere must have an adequate heat shield to with...
The recent resurgence of interest in blunt-body atmospheric entry for applications such as aeroassis...
Stagnation point radiative heating rates for manned vehicles entering the earth's atmosphere at para...
Aerodynamic heating of conical vehicles entering earth atmosphere at speeds greater than earth parab...
Long-range hypervelocity vehicles are studied in terms of their motion in powered flight, and their ...
A simplified analysis of the velocity and deceleration history of missiles entering the earth's atmo...
An analysis has been made of atmosphere entries for which the vehicle lift-drag ratio was modulated ...
The results of an analysis of the motion and heating during atmospheric reentry of manned space vehi...
An extensive, low-perigee orbital aerodynamic heating study was undertaken in support of the Atmosph...
This is a study of performance and control for transatmospheric (TAV) aerospace planes, that use ai...
A general method has been developed, using the methods of kinetic theory, whereby the surface temper...
Laboratory simulation of hypervelocity heat transfer problem during planetary entr
The dimensionless, transformed, nonlinear differential equation developed in NASA TR R-11 for descri...
The ballistic vehicle is found to be the least efficient of the several types studied in the sense t...
A differential evolutionary algorithm has been executed to optimize the hypersonic aerodynamic and s...
A spacecraft designed to operate in a planetary atmosphere must have an adequate heat shield to with...
The recent resurgence of interest in blunt-body atmospheric entry for applications such as aeroassis...