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NACA Advanced Confidential Reports
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Effect of leakage past aileron nose on aerodynamic characteristics of plain and internally balanced ailerons on NACA 66(215)-216, a = 1.0 airfoil
Wind-Tunnel Investigation of Control-Surface Characteristics: [Part] 18 - A Linked Overhang Aerodynamic Balance
Wind-tunnel investigation of control-surface characteristics 19: a double flap with an overhang and an internal aerodynamic balance
Wind-Tunnel Investigation of Shielded Horn Balances and Tabs on a 0.7-Scale Model of XF6F Vertical Tail Surface
Wind-tunnel investigation of control-surface characteristics 13: various flap overhangs used with a 30-percent-chord flap in an NACA 66-009 airfoil
Wind-tunnel data on the aerodynamic characteristics of airplane control surfaces
Flight tests of an all-movable vertical tail on the Fairchild XR2K-1 airplane
Scale and Turbulence Effects on the Lift and Drag Characteristics of the NACA 65(Sub 3)-418, A=1.0 Airfoil Section
Scale-effect tests in a turbulent tunnel of the NACA 65(sub 3)-418, a = 1.0 airfoil section with 0.20-airfoil-chord split flap
Lift and drag data for 30 pusher-propeller shaft housings on an NACA 65,3-018 airfoil section
Two-dimensional wind-tunnel investigation of 0.20-airfoil-chord plain ailerons of different contour on an NACA 65(sub 1)-210 airfoil section
Preliminary Report on Laminar-Flow Airfoils and New Methods Adopted for Airfoil and Boundary-Layer Investigations
Investigation of the Boundary Layer About a Symmetrical Airfoil in a Wind Tunnel of Low Turbulence
Wind-Tunnel Investigation of an NACA 66-Series 16-Percent-Thick Low-Drag Tapered Wing With Fowler and Split Flaps
Wind-Tunnel Investigation of Trimming Tabs on a Thickened and Beveled Aileron on a Tapered Low-Drag Wing
Effect of Compressibility on the Pressure and Forces Acting on a Modified NACA 65,3-019 Airfoil Having a 0.20-Chord Flap
Wind-Tunnel Investigation of a Low-Drag Airfoil Section with a Double Slotted Flap
Effects of Propellers and of Vibration on the Extent of Laminar Flow on the NACA 27-212 Airfoil
An Interim Report on the Stability and Control of Tailless Airplanes
An Analytical Investigation of the Effects of Elevator-Fabric Distortion on the Longitudinal Stability and Control of an Airplane
Determination of the Stability and Control Characteristics of a Tailless All-Wing Airplane Model with Sweepback in the Langley Free-Flight Tunnel
Effect of Wing Modifications on the Longitudinal Stability of a Tailless All-Wing Airplane Model
Experimental Investigation of a New Type of Low-Drag Wing-Nacelle Combination
The Effect of Streamlining the Aterbody of an N.A.C.A. Cowling
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