Add to ORKGLarge stiffened cylinders used in launch vehicles (LV), such as the Space Shuttle External Tank, are manufactured by welding multiple curved panel sections into complete cylinders. The effects of the axial weld lands between the panel sections on the buckling load were studied, along with the interaction between the acreage stiffener arrangement and the weld land geometry. This document contains the results of the studies
Compression tests on integrally stiffened cylinders - determination of loads and stresses associated...
Four honeycomb sandwich panel types, representing 1/16th arc segments of a 10-m diameter barrel sect...
From the 1920s to the early 1970s, many shell buckling experiments were conducted in an effort to un...
Results from the testing of cylinder test article SBKF-P2-CYLTA01 (referred to herein as TA01) are p...
The NASA Engineering Safety Center (NESC) Shell Buckling Knockdown Factor Project (SBKF) was establi...
Results from the buckling test of a compression-loaded 8-ft-diameter seamless (i.e., without manufac...
A summary of a NASA design analysis and test program on the buckling of large-scale, integrally-stif...
A curvilinear stiffened panel was designed, manufactured, and tested in the Combined Load Test Fixtu...
A curvilinear stiffened panel was designed, manufactured, and tested in the Combined Load Test Fixtu...
The integrally stiffened cylinder (ISC) process, pioneered by NASA Langley Research Center, offers s...
Buckling data review for stiffened cylinder failures during axial compression and bendin
Design and analysis results are reported for a panel that is a 16th arc-segment of a full 33-ft diam...
This report describes the analytical study of two full-scale tapered composite struts. The analytica...
Since its founding, NASA has been dedicated to the advancement of aeronautics and space science. The...
This report describes the development of a novel structural concept, Pultruded Rod Stitched Efficien...
Compression tests on integrally stiffened cylinders - determination of loads and stresses associated...
Four honeycomb sandwich panel types, representing 1/16th arc segments of a 10-m diameter barrel sect...
From the 1920s to the early 1970s, many shell buckling experiments were conducted in an effort to un...
Results from the testing of cylinder test article SBKF-P2-CYLTA01 (referred to herein as TA01) are p...
The NASA Engineering Safety Center (NESC) Shell Buckling Knockdown Factor Project (SBKF) was establi...
Results from the buckling test of a compression-loaded 8-ft-diameter seamless (i.e., without manufac...
A summary of a NASA design analysis and test program on the buckling of large-scale, integrally-stif...
A curvilinear stiffened panel was designed, manufactured, and tested in the Combined Load Test Fixtu...
A curvilinear stiffened panel was designed, manufactured, and tested in the Combined Load Test Fixtu...
The integrally stiffened cylinder (ISC) process, pioneered by NASA Langley Research Center, offers s...
Buckling data review for stiffened cylinder failures during axial compression and bendin
Design and analysis results are reported for a panel that is a 16th arc-segment of a full 33-ft diam...
This report describes the analytical study of two full-scale tapered composite struts. The analytica...
Since its founding, NASA has been dedicated to the advancement of aeronautics and space science. The...
This report describes the development of a novel structural concept, Pultruded Rod Stitched Efficien...
Compression tests on integrally stiffened cylinders - determination of loads and stresses associated...
Four honeycomb sandwich panel types, representing 1/16th arc segments of a 10-m diameter barrel sect...
From the 1920s to the early 1970s, many shell buckling experiments were conducted in an effort to un...