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Langley Aeronautical Laboratory
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Buckling (Mechanics)
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1
Effect of normal pressure on the critical compressive and shear stress of curved sheet /
by
Rafel, Norman
Published 1945
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2
Effect of normal pressure on the critical compressive stress of curved sheet /
by
Rafel, Norman
Published 1942
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Charts for calculation of the critical compressive stress for local instability of idealized web- and T-stiffened panels /
by
Boughan, Rolla B.
Published 1944
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4
Critical stress for an infinitely long flat plate with elastically restrained edges under combined shear and direct stress /
by
Stowell, Elbridge Z.
Published 1943
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Principles of moment distribution applied to stability of structures composed of bars or plates /
by
Lundquist, Eugene E.
Published 1948
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Tables of stiffness and carry-over factor for flat rectangular plates under compression /
by
Kroll, W. D.
Published 1943
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7
The effect of internal pressure on the buckling stress of thin-walled circular cylinders under torsion /
by
Crate, Harold
,
Batdorf, S. B.
,
Baab, George W.
Published 1944
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Knovel (Firm)
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Langley Aeronautical Laboratory
United States. National Advisory Committee for Aeronautics
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Baab, George W.
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2
Rafel, Norman
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2
Stowell, Elbridge Z.
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2
Batdorf, S. B.
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Boughan, Rolla B.
1 results
1
Crate, Harold
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Kroll, W. D.
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Lundquist, Eugene E.
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Sandlin, Charles W.
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Schuette, Evan H.
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Schwartz, Edward B.
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Language
English
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