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National Advisory Committee for Aeronautics Collection
780
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National Advisory Committee for Aeronautics Collection
780
Technical Report Archive and Image Library
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NACA Research Memorandums
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NACA Technical Memorandums
16
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NACA Research Memorandums
470
NACA Technical Notes
247
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1955
780
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1955
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National Advisory Committee for Aeronautics Collection
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Wind-Tunnel Investigation at Low Speed of a Wing Having 63 Degree Sweepback and a Drooped Tip
Development of a new flutter testing technique using a towed dynamic airplane model equipped with an automatic stabilizing system: Experimental and calculated dynamic stability characteristics for speeds up to 200 mph
Simulator studies of a simple homing system
An Investigation of Loads on Ailerons at Transonic Speeds
Wind-Tunnel Investigation at Low Speed of Sideslipping, Rolling, Yawing, and Pitching Characteristics for a Model of a 45 Degree Swept-Wing Fighter-Type Airplane
An Experimental Investigation of the Flow Phenomena Over Bodies at High Angles of Attack at a Mach Number of 2.01
Wing-load measurements at supersonic speeds of the Douglas D-558-II research airplane
Statistical measurements of landing contact conditions of the Boeing B-47 airplane
Modified tubular combustor as high-temperature gas generators
An experimental investigation of the unsteady lift induced on a wing in the downwash field of an oscillating canard control surface
Estimation of Incremental Pitching Moments Due to Trailing-Edge Flaps on Swept and Triangular Wings
Aerodynamic heating of rocket-powered research vehicles at hypersonic speeds
Simplified procedures for estimating flap-control loads at supersonic speeds
Force and Pressure Measurements on Several Canopy-Fuselage Configurations at Transonic Mach Numbers 1.41 and 2.01
Component Operating Trends During Acceleration and Deceleration of Two Hypothetical Two-Spool Turbojet Engines
Wing Pressure Distributions Over the Lift Range of the Convair XF92A Delta-Wing Airplane at Subsonic and Transonic Speeds
Ditching investigation of a 1/25-scale model of a 255,000-pound transport airplane
Investigation of some wake vortex characteristics of an inclined ogive-cylinder body at Mach number 1.98
Investigation of Equilibrium Temperatures and Average Laminar Heat-Transfer Coefficients for the Front Half of Swept Circular Cylinders at a Mach Number of 6.9
Preliminary performance data of several tail-pipe-cascade-type model thrust reversers
Theoretical Investigation of Laminar Heat Transfer on Yawed Infinite Cylinders in Supersonic Flow and a Comparison With Experimental Data
Experimental investigation of a transonic compressor rotor with a 1.5-inch chord length and an aspect ratio of 3.0 2: blade-element performance
Some Effects of Fluid in Pylon-Mounted Tanks on Flutter
The Unsteady Normal-Force Characteristics of Selected NACA Profiles at High Subsonic Mach Numbers
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