1. M. V. Hyatt and M. O. Speidel:Stress Corrosion Cracking in High Strength Steels and in Titanium and Aluminum Alloys, Chap. 4, B. F. Brown, ed., U.S. Gov. Printing Off., No. 0851-0058, Washington, D.C., 1972.
2. M. V. Hyatt and H. W. Schimmelbusch:Development of a High-Strength Stress-Corrosion-Resistant Aluminum Alloy for Use in Thick Sections, 167 pp., Air Force Materials Lab. Tech. Report AFML-TR-70–109, 1970.
3. C. F. Babilon, R. H. Wygonik, G. E. Nordmark, and B. W. Lifka:Mechanical Properties, Fracture Toughness, Fatigue, Environmental Fatigue Crack Growth Rates and Corrosion Characteristics of High Toughness Aluminum Alloy Forgings, Sheet and Plate, 226 pp., Air Force Materials Lab. Tech. Report AFML-TR-73–83, 1973.
4. M. V. Hyatt:Program to Improve the Fracture Toughness and Fatigue Resistance of Aluminum Sheet and Plate for Airframe Applications, 198 pp., Air Force Materials Lab. Tech. Report AFML-TR-73–224, 1973.
5. P. J. Blau:Effect of Iron and Silicon Content on Stress Corrosion Cracking in a Thermomechanically Processed Aluminum Alloy, 34 pp., Air Force Materials Lab. Tech. Report AFML-TR-75-215, 1975.