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Number of records: 8.
Matthews Jr., James T. (1948) Effect of Downwash on the Estimated Elevator Deflection Required for Trim of the XS-1 Airplane at Supersonic Speeds. Technical Report NACA RM L8H06a, Research Engineering, NASA Dryden Flight Research Center.
Williams, Walter C. (1948) Limited Measurements of Static Longitudinal Stability in Flight of Douglas D-558-I Airplane. Technical Report NACA RM L8E14, Research Engineering, NASA Dryden Flight Research Center.
Beeler, De E. and McLaughlin, Milton D. and Clift, Dorothy C. (1948) Measurements of the Chordwise Pressure Distributions Over the Wing of the XS-1 Research Airplane in Flight. Technical Report NACA RM L8G21, Research Engineering, NASA Dryden Flight Research Center.
Drake, Hubert M. and Goodman, Harold R. and Hoover, Herbert H. (1948) Preliminary Results of NACA Transonic Flights of the XS-1 Airplane with 10-Percent-Thick Wing and 8-Percent-Thick Horizontal Tail. Technical Report NACA RM L8I29, Research Engineering, NASA Dryden Flight Research Center.
McLaughlin, Milton D. and Clift, Dorothy C. (1948) Results Obtained During a Dive Recovery of the Bell XS-1 Airplane to High Lift Coefficients at a Mach Number Greater than 1.0. Technical Report NACA RM L8C23a, Research Engineering, NASA Dryden Flight Research Center.
Drake, Hubert M. and McLaughlin, Milton D. and Goodman, Harold R. (1948) Results Obtained During Accelerated Transonic Tests of the Bell XS-1 Airplane in Flights to a Mach Number of 0.92. Technical Report NACA RM L8A05a, Research Engineering, NASA Dryden Flight Research Center.
Goodman, Harold R. and Drake, Hubert M. (1948) Results Obtained During Extension of U.S. Air Force Transonic-Flight Tests of XS-1 Airplane. Technical Report NACA RM L8I28, Research Engineering, NASA Dryden Flight Research Center.
Williams, W. C. and Beeler, De E. (1948) Results of Preliminary Flight Tests of the XS-1 Airplane (8-Percent Wing) to a Mach Number of 1.25. Technical Report NACA RM L8A23a, Research Engineering, NASA Dryden Flight Research Center.
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