Sandwich cylinder instability under nonuniform axial stress
- 1 February 1964
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 2 (2), 398-399
- https://doi.org/10.2514/3.2293
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- THERMAL STRESS DETERMINATION TECHNIQUES FOR SUPERSONIC TRANSPORT AIRCRAFT STRUCTURES. PART II DESIGN DATA FOR SANDWICH PLATES AND CYLINDERS UNDER APPLIED LOADS AND THERMAL GRADIENTSPublished by Defense Technical Information Center (DTIC) ,1964
- Effect of Dissociation on the Rate of Vibrational RelaxationPhysics of Fluids, 1962
- Elastic Instability of a Cylindrical Shell Under Arbitrary Circumferential Variation of Axial StressJournal of the Aerospace Sciences, 1960
- Thermal Buckling of Circular Cylindrical Shells Under Circumferential Temperature GradientsJournal of the Aerospace Sciences, 1959
- BUCKLING OF CYLINDERS OF SANDWICH CONSTRUCTION IN AXIAL COMPRESSIONPublished by Defense Technical Information Center (DTIC) ,1957
- Buckling of Sandwich Cylinders Under Axial CompressionJournal of the Aeronautical Sciences, 1951