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  Partner: UNT Libraries Government Documents Department
 Serial/Series Title: NACA Advanced Restricted Report
 Collection: National Advisory Committee for Aeronautics Collection
Charts for calculation of the critical compressive stress for local instability of idealized web- and T-stiffened panels

Charts for calculation of the critical compressive stress for local instability of idealized web- and T-stiffened panels

Date: August 1, 1944
Creator: Baab, George W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Charts for calculation of the critical stress for local instability of columns with I-, Z-, channel and rectangular-tube section

Charts for calculation of the critical stress for local instability of columns with I-, Z-, channel and rectangular-tube section

Date: November 1, 1943
Creator: Heimerl, George J
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Charts for critical combinations of longitudinal and transverse direct stress for flat rectangular plates

Charts for critical combinations of longitudinal and transverse direct stress for flat rectangular plates

Date: March 1, 1946
Creator: Stein, Manuel
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Charts for determining jet-boundary corrections for complete models in 7- by 10-foot closed rectangular wind tunnels

Charts for determining jet-boundary corrections for complete models in 7- by 10-foot closed rectangular wind tunnels

Date: September 1, 1945
Creator: Gray, Joseph L , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Charts for the minimum-weight design of 24S-T aluminum-alloy flat compression panels with longitudinal Z-section stiffeners

Charts for the minimum-weight design of 24S-T aluminum-alloy flat compression panels with longitudinal Z-section stiffeners

Date: August 1, 1945
Creator: Schuette, Evan H
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Column and plate compressive strengths of aircraft structural materials : 17S-T aluminum-alloy sheet

Column and plate compressive strengths of aircraft structural materials : 17S-T aluminum-alloy sheet

Date: June 1, 1945
Creator: Roy, J Albert
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Column and Plate Compressive Strengths of Aircraft Structural Materials: 24S-T Aluminum-alloy Sheet

Column and Plate Compressive Strengths of Aircraft Structural Materials: 24S-T Aluminum-alloy Sheet

Date: June 1, 1945
Creator: Lundquist, Eugene E.; Schuette, Evan H.; Heimerl, George J. & Roy, J. Albert
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Column and plate compressive strengths of aircraft structural materials : extruded 14S-T aluminum alloy

Column and plate compressive strengths of aircraft structural materials : extruded 14S-T aluminum alloy

Date: May 1, 1946
Creator: Niles, Donald E
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Column and plate compressive strengths of aircraft structural materials : extruded 24S-T aluminum alloy

Column and plate compressive strengths of aircraft structural materials : extruded 24S-T aluminum alloy

Date: July 1, 1945
Creator: Roy, J Albert
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Column and Plate Compressive Strengths of Aircraft Structural Materials: Extruded 24S-T Aluminum Alloy

Column and Plate Compressive Strengths of Aircraft Structural Materials: Extruded 24S-T Aluminum Alloy

Date: July 1, 1945
Creator: Heimerl, George J. & Roy, J Albert
Description: Column and plate compressive strengths of extruded 24S-T aluminum alloy were determined both within and beyond the elastic range from tests of thin-strip columns and local-instability tests of H-, Z-,and channel-section columns. These tests are part of an extensive research investigation to provide data on the' structural strength of various aircraft materials. The results are presented in the form of curves and charts that are suitable for use in the design and analysis of aircraft structures.
Contributing Partner: UNT Libraries Government Documents Department