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NACA Advanced Restricted Reports
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Analysis of Wind-Tunnel Stability and Control Tests in Terms of Flying Qualities in Full-Scale Airplanes
The effect of compressibility on two-dimensional tunnel-wall interference for a symmetrical airfoil
The Flow of a Compressible Fluid Past a Curved Surface
Wind Tunnel Investigation of Control-Surface Characteristics 11: Various Large Overhang and Internal-Type Aerodynamic Balances for a Straight- Contour Flap on the NACA 0015 Airfoil
Wind Tunnel Investigation of Control Surface Characteristics: [Part] 12 - Various Cover-Plate Alinements on the NACA 0015 Airfoil With a 30 Percent Chord Flap and Large Sealed Internal Balance
Theory and preliminary flight tests of an all-movable vertical tail surface
Wind-Tunnel Investigation of a Full-Span Retractable Flap in Combination With Full-Span Plain and Internally Balanced Ailerons on a Tapered Wing
Wind-tunnel tests of two tapered wings with straight leading edges and with constant-chord center sections of different spans
Aerodynamic characteristics and flap loads of perforated double split flaps on a rectangular NACA 23012 airfoil
Wind-Tunnel Investigation of an NACA 23012 Airfoil With a 0.30-Airfoil-Chord Double Slotted Flap
Critical shear stress of an infinitely long flat plate with equal elastic restraints against rotation along the parallel edges
Full-scale tunnel investigation of the pressure distribution over the tail of the P-47B airplane
Wind-Tunnel Investigation of a Plain Aileron with Various Trailing-Edge Modifications on a Tapered Wing 3: Ailerons with Simple and Spring-Linked Balancing Tabs
Wind-Tunnel Investigation of the Characteristics of Blunt-Nose Ailerons on a Tapered Wing
Some Systematic Model Experiments of the Bow-Spray Characteristics of Flying-Boat Hulls Operating at Low Speeds in Waves
An investigation of aircraft heaters 13: performance of corrugated and noncorrugated fluted type exhaust gas-air heat exchangers
Aerodynamic and Hydrodynamic Tests of a Family of Models of Flying-Boat Hulls Derived From a Streamline Body: NACA Model 84 Series
Wind-tunnel tests of four full-scale seaplane floats
An investigation of aircraft heaters 10: measured and predicted performance of a fluted-type exhaust gas and air heat exchanger
An investigation of aircraft heaters 11: measured and predicted performance of a slotted-fin exhaust gas and air heat exchanger
An Investigation of Aircraft Heaters 8: A Simplified Method for the Calculation of the Unit Thermal Conductance Over Wings
Wind-Tunnel Investigation of Control-Surface Characteristics 14: NACA 0009 Airfoil With a 20-Percent-Chord Double Plain Flap
Flight Tests of Various Tail Modifications on the Brewster XSBA-1 Airplane 1: Measurements of Flying Qualities With Original Tail Surfaces
Experimental Determination of the Yawing Moment Due to Yawing Contributed by the Wing, Fuselage, and Vertical Tail of a Midwing Airplane Model
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