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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

Analysis of V-G records from ten types of Navy airplanes in squadron operations during the period 1949 to 1953

A study of service-imposed maneuvers of four jet fighter airplanes in relation to their handling qualities and calculated dynamic characteristics

Applications of power spectral analysis methods to maneuver loads obtained on jet fighter airplanes during service operations

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

The Frequency Content of the Control Input and Airplane Response Obtained During Service Operations of Fighter Airplanes


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