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- Flight measurements with the Douglas D-558-II (BuAero No. 37974) research airplane : determination of the aerodynamic center and zero-lift pitching-moment coefficient of the wing-fuselage combination by means of tail-load measurements in the Mach num
- Flight Measurements With the Douglas D-558-II (BuAero No. 37974) Research Airplane: Measurements of the Buffet Boundary and Peak Airplane Normal-Force Coefficients at Mach Numbers Up to 0.90
- Flight Measurements With the Douglas D-558-II (BuAero No. 37974) Research Airplane: Measurements of Wing Loads at Mach Numbers Up to 0.87
- Flight Measurements With the Douglas D-558-II (BuAero No. 37974) Research Airplane: Measurements of the Distribution of the Aerodynamic Load Among the Wing, Fuselage, and Horizontal Tail at Mach Numbers Up to 0.87
- Division of Load Among the Wing, Fuselage, and Tail of Aircraft
- Preliminary Results From a Limited Investigation of the Use of Controls During Service Operational Training With Fighter Airplanes
- A study of the use of controls and the resulting airplane response during service training operations of four jet fighter airplanes
- A study of means for rationalizing airplane design loads
- A study of service-imposed maneuvers of four jet fighter airplanes in relation to their handling qualities and calculated dynamic characteristics
- Analysis of V-G records from ten types of Navy airplanes in squadron operations during the period 1949 to 1953
- Applications of power spectral analysis methods to maneuver loads obtained on jet fighter airplanes during service operations
- The Frequency Content of the Control Input and Airplane Response Obtained During Service Operations of Fighter Airplanes
- Notes on a Large-Scale Statistical Program for the Establishment of Maneuver-Loads Design Criteria for Military Airplanes
- Time-History Data of Maneuvers Performed by a Republic F-84F Airplane During Squadron Operational Training
