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NACA Research Memorandums
269
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NACA Research Memorandums
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1949
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1949
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Determination of Rate, Area, and Distribution of Impingement of Waterdrops on Various Airfoils From Trajectories Obtained on the Differential Analyzer
Determination of rate, area, and distribution of impingement of of waterdrops on various airfoils from trajectories obtained on the differential analyzer
A review of instruments developed for the measurement of the meteorological factors conductive to aircraft icing
An Electric Thrust Meter Suitable for Flight Investigation of Propellers
Investigation of the Kingfisher XAUM-2 Flying Torpedo in the Langley Full Scale Tunnel, TED No. NACA DE 327
Downwash in Vortex Region Behind Trapezoidal-Wing Tip at Mach Number 1.91
Wing-tunnel investigation at low transonic speeds of the effects of number of wings on the lateral-control effectiveness of an RM-5 test vehicle
Spin-Tunnel Investigation of the Jettisoning of External Fuel Tanks in Spins
Analytical determination of effect of water injection on power output of turbine-propeller engine
Comparative Tests of the Rolling Effectiveness of Constant-Chord, Full-Delta, and Half-Delta Ailerons on Delta Wings at Transonic and Supersonic Speeds
Low-Speed Investigation of Deflectable Wing-Tip Ailerons on an Untapered 45 Degrees Sweptback Semispan Wing With and Without an End Plate
An Analysis of Airspeeds Attained by a Douglas DC-4 Airplane in Commercial Operations During the Early Months of 1947
Two-Dimensional Wind-Tunnel Investigation of Two NACA 7-Series Type Airfoils Equipped With a Slot-Lip Aileron, Trailing-Edge Frise Aileron, and a Double Slotted Flap
Aerodynamic characteristics of a flying-boat hull having a length-beam ratio of 15 and a warped forebody
Preliminary full-scale investigation of a 1/3-scale model of a convertible-type airplane
Longitudinal Stability and Control Characteristics of a Semispan Wind-Tunnel Model of a Tailless Airplane and a Comparison With Complete-Model Wind-Tunnel Tests and Semispan-Model Wing-Flow Tests
Comparison of performance of AN-F-58 and AN-F-32 fuels in J33-A-23 turbojet engine
Aerodynamic characteristics of a wing with quarter-chord line swept back 35 degrees, aspect ratio 4, taper ratio 0.6, and NACA 65A006 airfoil section: Transonic-bump method
Low-Speed Investigation of Aileron and Spoiler Characteristics of a Wing Having 42 Degrees Sweepback of the Leading Edge and Circular-Arc Airfoil Sections at Reynolds Numbers of Approximately 6.0 X 10(Exp 6)
Measurements of Aileron Effectiveness of Bell X-1 Airplane Up to a Mach Number of 0.82
Wind-tunnel investigation of transonic aileron flutter
Aerodynamic characteristics of a 6-percent-thick symmetrical double-wedge airfoil at transonic speeds from tests by the NACA wing-flow method
Investigations of an Annular Diffuser-Fan Combination Handling Rotating Flow
Hydrodynamic characteristics of a swept planing-tail hull
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