Influence of edge conditions on the stability of axially compressed cylindrical shells /

An engineering procedure for calculating compressive strength of isogrid cylindrical shells with buckled skin /

Heard, Walter L.
Slysh, Paul, joint author.
Anderson, Melvin S., joint author.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1976

Cover title.Includes bibliographical references (p. 16).Mode of access: Internet

Stability investigation of a blunted cone and a blunted ogive with a flared cylinder afterbody at mach numbers from 0.30 to 2.85 / Lucille C. Coltrane.

Coltrane, Lucille C.
United States. National Aeronautics and Space Administration.

Cover title."November 1959."Includes bibliographical references.Mode of access: Internet

Buckling tests of three 4.6 meter diameter aluminum honeycomb sandwich conical shells loaded under external pressure /

Anderson, James Kent.
Davis, Randall C.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 14).Mode of ...

Creep bending and buckling of thin circular cylindrical shells /

Erickson, Burton.
Polytechnic Institute of Brooklyn.

January 1960

"NASA TN D-429.""Polytechnic Institute of Brooklyn.""June 1960."Cover title.Includes bibliographical...

Deformations and stresses in circular cylindrical shells caused by pipe attachment.

Kempner, J.
Knolls Atomic Power Laboratory.
General Electric Company.
U.S. Atomic Energy Commission.

"KAPL-926.""June 1953."Includes bibliographical references (page 31).U.S. Atomic Energy Commission C...

Structural behavior of pressurized, ring-stiffened, thin-wall cylinders subjected to axial compression /

Peterson, James P.
Dow, Marvin B.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Stresses and loads; Structures.Includes bibliographical references.Mode o...

Stresses in a compressively loaded circular semimonocoque cylinder with a cutout /

Martin, R. E.
Manned Spacecraft Center (U.S.)

January 1967

"NASA TM X-1354.""Manned Spacecraft Center.""February 1967"--Cover.Includes bibliographical referenc...

Effects of configuration modifications on aerodynamic characteristics of tension shell shapes at Mach 3.0 /

Sawyer, James Wayne, 1941-
Deveikis, William D.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."August 1967."Includes bibliographical references (p. 11).Mode of access: Internet

Plastic instability of cylindrical shells with rigid end closures : topical report /

Salmon, M. A.
IIT Research Institute
U.S. Atomic Energy Commission.

"IITRI-528-19 ; UC-80 ; TID-4500 (32nd Ed.)."Includes bibliographical references (p. 97).U.S. Atomic...

Bending strength of a large thin-walled pressure-stabilized cylinder beyond onset of compressive skin wrinkling /

Miller, Robert P.
Gerus, Theodore.
Lewis Research Center.

January 1966

"NASA TM X-1311.""Lewis Research Center, Cleveland, Ohio.""November 1966"--Cover.Includes bibliograp...

Analysis of frame-reinforced cylindrical shells,

MacNeal, Richard H.
Bailie, John A., joint author.

January 1960

Errata slips inserted."Originally prepared as LMSD 49732, Lockheed Missiles and Space Division, Sunn...

Combinations of temperature and axial compression required for buckling of a ring-stiffened cylinder /

Anderson, Melvin S.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Stresses and loads; Structures.Includes bibliographical references.Mode of ...

The influence of the boundary conditions on the buckling load of cylindrical shells under axial compression

Kobayashi, S.

August 1966

Influence of boundary conditions of buckling load of cylindrical shells under axial compressio

Minimum weight design of axially compressed ring and stringer stiffened cylindrical shells /

Block, David L.
Langley Research Center.
Florida Technological University.

January 1971

This report investigates the minimum weight design of axially compressed ring and stringer stiffened...

A digital computer method for design and analysis of axisymmetric thin shells subjected to pressure and thermal environments /

Neudecker, J. W.
U.S. Atomic Energy Commission.
Los Alamos Scientific Laboratory.

January 1964

"Report written: April 1, 1964 ; Report distributed: November 17, 1964.""Contract W-7405-ENG.36 with...

An engineering procedure for calculating compressive strength of isogrid cylindrical shells with buckled skin /

Heard, Walter L.
Slysh, Paul, joint author.
Anderson, Melvin S., joint author.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1976

Cover title.Includes bibliographical references (p. 16).Mode of access: Internet

Stability investigation of a blunted cone and a blunted ogive with a flared cylinder afterbody at mach numbers from 0.30 to 2.85 / Lucille C. Coltrane.

Coltrane, Lucille C.
United States. National Aeronautics and Space Administration.

Cover title."November 1959."Includes bibliographical references.Mode of access: Internet

Buckling tests of three 4.6 meter diameter aluminum honeycomb sandwich conical shells loaded under external pressure /

Anderson, James Kent.
Davis, Randall C.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 14).Mode of ...

Creep bending and buckling of thin circular cylindrical shells /

Erickson, Burton.
Polytechnic Institute of Brooklyn.

January 1960

"NASA TN D-429.""Polytechnic Institute of Brooklyn.""June 1960."Cover title.Includes bibliographical...

Deformations and stresses in circular cylindrical shells caused by pipe attachment.

Kempner, J.
Knolls Atomic Power Laboratory.
General Electric Company.
U.S. Atomic Energy Commission.

"KAPL-926.""June 1953."Includes bibliographical references (page 31).U.S. Atomic Energy Commission C...

Structural behavior of pressurized, ring-stiffened, thin-wall cylinders subjected to axial compression /

Peterson, James P.
Dow, Marvin B.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Stresses and loads; Structures.Includes bibliographical references.Mode o...

Stresses in a compressively loaded circular semimonocoque cylinder with a cutout /

Martin, R. E.
Manned Spacecraft Center (U.S.)

January 1967

"NASA TM X-1354.""Manned Spacecraft Center.""February 1967"--Cover.Includes bibliographical referenc...

Effects of configuration modifications on aerodynamic characteristics of tension shell shapes at Mach 3.0 /

Sawyer, James Wayne, 1941-
Deveikis, William D.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."August 1967."Includes bibliographical references (p. 11).Mode of access: Internet

Plastic instability of cylindrical shells with rigid end closures : topical report /

Salmon, M. A.
IIT Research Institute
U.S. Atomic Energy Commission.

"IITRI-528-19 ; UC-80 ; TID-4500 (32nd Ed.)."Includes bibliographical references (p. 97).U.S. Atomic...

Bending strength of a large thin-walled pressure-stabilized cylinder beyond onset of compressive skin wrinkling /

Miller, Robert P.
Gerus, Theodore.
Lewis Research Center.

January 1966

"NASA TM X-1311.""Lewis Research Center, Cleveland, Ohio.""November 1966"--Cover.Includes bibliograp...

Analysis of frame-reinforced cylindrical shells,

MacNeal, Richard H.
Bailie, John A., joint author.

January 1960

Errata slips inserted."Originally prepared as LMSD 49732, Lockheed Missiles and Space Division, Sunn...

Combinations of temperature and axial compression required for buckling of a ring-stiffened cylinder /

Anderson, Melvin S.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Stresses and loads; Structures.Includes bibliographical references.Mode of ...

The influence of the boundary conditions on the buckling load of cylindrical shells under axial compression

Kobayashi, S.

August 1966

Influence of boundary conditions of buckling load of cylindrical shells under axial compressio

Minimum weight design of axially compressed ring and stringer stiffened cylindrical shells /

Block, David L.
Langley Research Center.
Florida Technological University.

January 1971

This report investigates the minimum weight design of axially compressed ring and stringer stiffened...

A digital computer method for design and analysis of axisymmetric thin shells subjected to pressure and thermal environments /

Neudecker, J. W.
U.S. Atomic Energy Commission.
Los Alamos Scientific Laboratory.

January 1964

"Report written: April 1, 1964 ; Report distributed: November 17, 1964.""Contract W-7405-ENG.36 with...

An engineering procedure for calculating compressive strength of isogrid cylindrical shells with buckled skin /

Heard, Walter L.
Slysh, Paul, joint author.
Anderson, Melvin S., joint author.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1976

Cover title.Includes bibliographical references (p. 16).Mode of access: Internet

Stability investigation of a blunted cone and a blunted ogive with a flared cylinder afterbody at mach numbers from 0.30 to 2.85 / Lucille C. Coltrane.

Coltrane, Lucille C.
United States. National Aeronautics and Space Administration.

Cover title."November 1959."Includes bibliographical references.Mode of access: Internet

Buckling tests of three 4.6 meter diameter aluminum honeycomb sandwich conical shells loaded under external pressure /

Anderson, James Kent.
Davis, Randall C.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 14).Mode of ...

Influence of edge conditions on the stability of axially compressed cylindrical shells /

Abstract

Extracted data

Influence of edge conditions on the stability of axially compressed cylindrical shells /

Abstract

Extracted data

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