v. 1. Methods of predicting structural temperatures due to aerodynamic heating, by A. H. Blessing.--v. 2. Aerodynamics, by J. R. Batt.--v. 3. Experimental and analytical methods for the determination of thermally-affected wing deflectional behavior, by R. H. Gallagher.--v. 3, sup. Description and results of tests conducted to determine the thermally affected behavior of corrugated multiweb wing structures, by J. F. Quinn.Mode of access: Internet
In this paper, a coupled aerothermoelastic dynamic stability analysis of a functionally-graded compo...
Compilation of methods of solution for thermal stress problems of types frequently encountered by ai...
Procedures for and results of aeroservothermoelastic studies are described. The objectives of these ...
According to the title of this lecture, two subjects will be covered, both of which are traditionall...
This work-in-progress presentation describes an ongoing research activity at the NASA Langley Resear...
The malfunction of thermal protection system (TPS) caused by aerodynamic heating is a latent trouble...
Thermal stresses, which may result from transient heating, can cause changes in the effective stiffn...
The structural effects of nonuniform temperature distributions, such as those produced by aerodynami...
Radiant heating experiments were performed in the laboratory on an instrumented multispar wing struc...
Analytical methods are described for the prediction of aerothermoelastic stability of hypersonic air...
This dissertation describes the aeroelastic analysis of a typical section, as well as the more compl...
Hypersonic aircraft design is a pressing area of research. The motivation to create aircraft that ca...
A methodology for obtaining shape sensitivities of flutter eigenvalues of aerothermoe-lastic structu...
Thermal stresses, which may result from transient heating, can cause changes in the effective stiffn...
This paper comprehensively reviews the progress of static aeroelastic effect prediction and correcti...
In this paper, a coupled aerothermoelastic dynamic stability analysis of a functionally-graded compo...
Compilation of methods of solution for thermal stress problems of types frequently encountered by ai...
Procedures for and results of aeroservothermoelastic studies are described. The objectives of these ...
According to the title of this lecture, two subjects will be covered, both of which are traditionall...
This work-in-progress presentation describes an ongoing research activity at the NASA Langley Resear...
The malfunction of thermal protection system (TPS) caused by aerodynamic heating is a latent trouble...
Thermal stresses, which may result from transient heating, can cause changes in the effective stiffn...
The structural effects of nonuniform temperature distributions, such as those produced by aerodynami...
Radiant heating experiments were performed in the laboratory on an instrumented multispar wing struc...
Analytical methods are described for the prediction of aerothermoelastic stability of hypersonic air...
This dissertation describes the aeroelastic analysis of a typical section, as well as the more compl...
Hypersonic aircraft design is a pressing area of research. The motivation to create aircraft that ca...
A methodology for obtaining shape sensitivities of flutter eigenvalues of aerothermoe-lastic structu...
Thermal stresses, which may result from transient heating, can cause changes in the effective stiffn...
This paper comprehensively reviews the progress of static aeroelastic effect prediction and correcti...
In this paper, a coupled aerothermoelastic dynamic stability analysis of a functionally-graded compo...
Compilation of methods of solution for thermal stress problems of types frequently encountered by ai...
Procedures for and results of aeroservothermoelastic studies are described. The objectives of these ...