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Decade:
1950-1959 (1)
1940-1949 (172)
1930-1939 (18)
1920-1929 (44)
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Serial/Series Title:
NACA Advanced Confidential Report (173)
NACA Wartime Reports (144)
NACA Special Report (15)
NACA Memorandum Report (3)
NACA Technical Reports (2)
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UNT Libraries Government Documents Department
Serial/Series Title:
NACA Aircraft Circulars
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The Supersonic Axial-Flow Compressor
Extension of Useful Operating Range of Axial-Flow Compressors by Use of Adjustable Stator Blades
Correlation of Wright Aeronautical Corporation cooling data on the R-3350-14 intermediate engine and comparison with data from the Langley 16-foot high-speed tunnel
Paths of Target Seeking Missiles in Two Dimensions
Paths of target-seeking missiles in two dimensions
Parameters determining performance of supersonic pilotless airplanes powered by ram-compression power planes
Investigations on laminar boundary-layer stability and transition on curved boundaries
Stability and control force tests of four- and six-unit wing designs of low aspect ratio and 20 degree triangular plan form
Critical Mach Numbers of Thin Airfoil Sections with Plain Flaps
Field of Flow About a Jet and Effect of Jets on Stability of Jet-Propelled Airplanes
Approximate formulas for the computation of turbulent boundary-layer momentum thicknesses in compressible flows
Development of Wing Inlets
Flight Investigation at High Speeds of Profile Drag of Wing of a P-47D Airplane Having Production Surfaces Covered with Camouflage Paint
Flight investigation at high speeds of profile drag of wing of a P-47D airplane having production surfaces covered with camouflage paint
A method for the calculation of external lift, moment, and pressure drag of slender open-nose bodies of revolution at supersonic speeds
Theory and application of hot-wire instruments in the investigation of turbulent boundary layers
Determination of the stability and control characteristics of a straight-wing, tailless fighter-airplane model in the Langley free-flight tunnel
Effects of specific types of surface roughness on boundary-layer transition
Effects of specific types of surface roughness on boundary-layer transition
Occurrence of iron oxides on cast-iron engine surfaces after operation
Effect of Compressibility on the Pressure and Forces Acting on a Modified NACA 65,3-019 Airfoil Having a 0.20-Chord Flap
The effect of wall interference upon the aerodynamic characteristics of an airfoil spanning a closed-throat circular wind tunnel
Wind-tunnel investigation of an NACA 66-series 16-percent-thick low-drag tapered wing with Fowler and split flaps
A flight investigation of NACA aileron modifications for the improvement of the lateral control characteristics of a high-speed fighter airplane
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