The Viking aeroshell is an extremely lightweight flexible shell structure that has undergone thorough buckling analyses in the course of its development. The analytical tools and modeling technique required to reveal the structural behavior are presented. Significant results are given which illustrate the complex failure modes not usually observed in simple models and analyses. Both shell-of-revolution analysis for the pressure loads and thermal loads during entry and a general shell analysis for concentrated tank loads during launch were used. In many cases fixes or alterations to the structure were required, and the role of the analytical results in determining these modifications is indicated
An assessment of the static strength of the Aeroassist Flight Experiment (AFE) Carrier Vehicle is pr...
Instruction manual for static structural analyses on shell-type spacecraft structure
Preliminary analysis showed that the doubly curved triangular shell elements were too stiff for thes...
The buckling modes of four optimized Mars entry aeroshell configurations at angle-of-attack loadings...
The buckling modes of four optimized Mars entry aeroshell configurations at angle-of-attack loadings...
A limited analytical investigation was conducted to assess the effects of structural elasticity on t...
A rigorous analytical study of cones stiffened by many thin-gage, open-section rings is presented. T...
The modified structure method, which is based on Koiter's theory of imperfections, was used to calcu...
Fracture mechanics methodology has developed rapidly over the past 10 years. Although not as yet suf...
The performance of the Viking lander has been evaluated by using a Monte Carlo simulation, and all r...
A summary of the existing NASA design criteria monographs for the design of buckling-resistant thin-...
This report investigates an analytical evaluation of buckling modes of shell configurations to deter...
From the 1920s to the early 1970s, many shell buckling experiments were conducted in an effort to un...
A variety of structural analyses have been performed on the Solid Rocket Boosters (SRB's) to provide...
Wind tunnel tests to determine aerodynamic characteristics of Viking spacecraft entry and lander con...
An assessment of the static strength of the Aeroassist Flight Experiment (AFE) Carrier Vehicle is pr...
Instruction manual for static structural analyses on shell-type spacecraft structure
Preliminary analysis showed that the doubly curved triangular shell elements were too stiff for thes...
The buckling modes of four optimized Mars entry aeroshell configurations at angle-of-attack loadings...
The buckling modes of four optimized Mars entry aeroshell configurations at angle-of-attack loadings...
A limited analytical investigation was conducted to assess the effects of structural elasticity on t...
A rigorous analytical study of cones stiffened by many thin-gage, open-section rings is presented. T...
The modified structure method, which is based on Koiter's theory of imperfections, was used to calcu...
Fracture mechanics methodology has developed rapidly over the past 10 years. Although not as yet suf...
The performance of the Viking lander has been evaluated by using a Monte Carlo simulation, and all r...
A summary of the existing NASA design criteria monographs for the design of buckling-resistant thin-...
This report investigates an analytical evaluation of buckling modes of shell configurations to deter...
From the 1920s to the early 1970s, many shell buckling experiments were conducted in an effort to un...
A variety of structural analyses have been performed on the Solid Rocket Boosters (SRB's) to provide...
Wind tunnel tests to determine aerodynamic characteristics of Viking spacecraft entry and lander con...
An assessment of the static strength of the Aeroassist Flight Experiment (AFE) Carrier Vehicle is pr...
Instruction manual for static structural analyses on shell-type spacecraft structure
Preliminary analysis showed that the doubly curved triangular shell elements were too stiff for thes...