Opening book details…
About this nonfiction
Increasing the compressive strength of 24S-T aluminum-alloy sheet by flexure rolling by Heimerl, George J. is a nonfiction available to read on EtoBox.
It is typically read by self-directed learners exploring a subject in depth.
Common subject areas: history, science, philosophy, social sciences.
- Author
- Heimerl, George J.
- Publisher
- National Advisory Committee for Aeronautics, 1946.
- Published
- 1946
- Language
- EN
- Category
- nonfiction
More by Heimerl, George J.
Browse all works by Heimerl, George J.
Similar books
- Elevated-temperature Compressive Stress-strain Data for 24S-T3 Aluminum-alloy Sheet and Comparisons with Extruded 75S-T6 Aluminum Alloy / William M. Roberts and George J. Heimerl. — William M. Roberts (1949)
- Column and Plate Compressive Strengths of Aircraft Structural Materials 24S-T Aluminum-alloy Sheet — Eugene E Lundquist; Langley Aeronautical Laboratory; United States (1945)
- Column and Plate Compressive Strengths of Aircraft Structural Materials Extruded 75S-T Aluminum-alloy — George J. Heimerl (1945)
- Fatigue Strength-stress Concentration Equation for Aluminum Alloy 24S-T3 — L. W. Hu (1967)
- Preliminary Investigation of the Compressive Strength and Creep Lifetime of 2024-T3 (formerly 24S-T3) Aluminum-alloy Plates at Elevated Temperatures / Eldon E. Mathauser and William D. Deveikis. — Eldon E. Mathauser (1955)
- Axial-load Fatigue Properties of 24S-T and 75S-T Aluminum Alloy as Determined in Several Laboratories — H. J Grover; W. S Hyler; Paul Kuhn; Charles B Landers; United States (1953)