External interference effects of a flow through static-pressure orifices of a NACA airspeed head at a Mach number of 3
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Silsby, Norman S↗
Engineering topics
Silsby, Norman S
Publications and source records attributed to Silsby, Norman S.
A summary of ground-loads statistics
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Westfall, John R↗
Statistical measurements of landing contact conditions of five military airplanes during routine daytime operations
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Silsby, Norman S↗
Landing conditions for large airplanes in routine operations
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Silsby, Norman S↗
Statistical measurements of landing-contact conditions of a heavy bomber
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Silsby, Norman S↗
Statistical Measurements of Contact Conditions of 478 Transport-airplane Landings During Routine Daytime Operations
Statistical measurements of contact conditions have been obtained, by means of a special photographic technique, of 478 landings of present-day transport airplanes made during routine daylight operations in clear air at the Washington National Airport. From the measurements, sinking speeds, rolling velocities, bank angles, and horizontal speeds at the instant before contact have been evaluated and a limited statistical analysis of the results has been made and is reported in this report.
Silsby, Norman S↗
Statistical measurements of contact conditions of 478 transport-airplane landings during routine daytime operations
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Silsby, Norman S↗
Distribution of lift and pitching moment between wing and fuselage and effects of wing flexibility and dive brake on a 1/30-scale semispan model of the Bell X-5 airplane at transonic speeds as determined by the NACA wing-flow method
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Morris, Garland J↗
Some measurements of landing contact conditions of transport airplanes in routine operations
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Silsby, Norman S↗
Longitudinal-control Effectiveness and Downwash Characteristics at Transonic Speeds of a 1/30-scale Semispan Model of the Bell X-5 Airplane as Determined by the NACA Wing-flow Method
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Silsby, Norman S↗
Investigation of the Distribution of Lift, Drag, and Pitching Moment Between the Wing and Fuselage of a 1/30-scale Semispan Model of the Bell X-5 Airplane at a Mach Number of 1.24 by the Naca Wing-flow Method
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Morris, Garland J↗
Contributions of Wing, Tail, and Fuselage to the Aerodynamic Characteristics of a Semispan Model of a Supersonic Airplane Configuration at Transonic Speeds from Tests by the NACA Wing-flow Method
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Silsby, Norman S↗
The Effect of Sweepback on the Longitudinal Characteristics at a Mach Number of 1.24 of a 1/30 Scale Semispan Model of the Bell X-5 Airplane from Tests by the NACA Wing Flow Method
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Morris, Garland J↗
Longitudinal Characteristics at Mach Number of 1.24 of 1/30-scale Semispan Model of Bell X-5 Variable-sweep Airplane with Wing Swept Back 60 Degrees : from Tests by NACA Wing-flow Method
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Silsby, Norman S↗
Longitudinal Stability and Control Characteristics of a Semispan Model of a Supersonic Airplane Configuration at Transonic Speeds from Tests by the NACA Wing-flow Method
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Silsby, Norman S↗
Comparative drag measurements at transonic speeds of 6-percent-thick airfoils of symmetrical double-wedge and circular-arc sections from tests by the NACA wing-flow method
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Silsby, Norman S↗
The effectiveness of a trailing-edge spoiler on a swept-back airfoil at transonic speeds from tests by the NACA wing-flow method
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Silsby, Norman S↗
Flight investigation of the effect of a local change in wing contour on chordwise pressure distribution at high speeds
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AIRPLANES, HIGH-SPEED↗