Design and Analysis of Subscale and Full-Scale Buckling-Critical Cylinders for Launch Vehicle Technology Development-Reference-Cited by-同舟云学术

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Design and Analysis of Subscale and Full-Scale Buckling-Critical Cylinders for Launch Vehicle Technology Development

Published:2012-04-23 Issue: Volume: Page:
ISSN:
Container-title:53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference<BR>20th AIAA/ASME/AHS Adaptive Structures Conference<BR>14th AIAA
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Author:

Hilburger Mark,Lovejoy Andrew,Thornburgh Robert,Rankin Charles

Publisher

American Institute of Aeronautics and Astronautics

Reference7 articles.

1. AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Honolulu, HI, Apr. 23-

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1. Investigation of Buckling Knockdown Factors for Pressurized Metallic Cylinders Using Various Numerical Modeling Techniques of Initial Imperfections;International Journal of Aeronautical and Space Sciences;2023-10-08

2. Critical circumferential wavelength of elastic buckling of longitudinal compressed thin-walled cylindrical shells;Scientific Reports;2023-10-04

3. Derivation of Buckling Knockdown Factors for Pressurized Orthogrid-Stiffened Cylinders of Launch Vehicle Structures;International Journal of Aeronautical and Space Sciences;2023-06-07

4. Post-buckling Partial Similitude Scaled Model for Stiffened Cylinders under Axial Compression by Energy Method;Buildings;2022-12-07

5. Buckling design of stiffened cylindrical shells under axial compression based on energy barrier approach;Thin-Walled Structures;2022-10

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