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National Advisory Committee for Aeronautics Collection
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Forces and moments on inclined bodies at Mach numbers from 3.0 to 6.3
Exploratory Investigation of Performance of Experimental Fuel-Rich Hydrogen Combustion System
Performance of a 20-inch steady-flow ram jet at high altitudes and ram-pressure ratios
Preliminary Free-Flight Investigation of the Effect of Airfoil Section on Aileron Rolling Effectiveness at Transonic and Supersonic Speeds
Pressure-distribution measurements on a full-scale horizontal tail surface for a Mach number range of 0.20 to 0.70
The use of perforated inlets for efficient supersonic diffusion
Wind-Tunnel Investigation of Bomb-Bay Configurations Intended to Minimize the Tumbling of Light-Weight Bombs
Lift and drag coefficients for the Bell X-1 airplane (8-percent-thick wing) in power-off transonic flight
Flight Investigation of the Longitudinal Stability and Control Characteristics of the Douglas D-558-I Airplane (BuAero No. 37972) at Mach Numbers Up to 0.89
Pressure-distribution measurements over a 45 degree sweptback wing at transonic speeds by the NACA wing-flow method
A study of the flow over a 45 degree sweptback wing-fuselage combination at transonic Mach numbers
Investigation in the Ames 12-Foot Pressure Wind Tunnel of a Model Horizontal Tail of Aspect Ratio 3 and Taper Ratio 0.5 Having the Quarter-Chord Line Swept Back 45 Degrees
Characteristics of Four Nose Inlets as Measured at Mach Numbers Between 1.4 and 2.0
Comparison of Zero-Lift Drag Determined by Flight Tests at Transonic Speeds of Pylon, Underslung, and Symmetrically Mounted Nacelles at 40 Percent Semispan of a 45 Degrees Sweptback Wing and Body Combination
Some observations on stall flutter and buffeting
Effect of Variations in Reynolds Number on the Aerodynamic Characteristics of Three Bomb or Store Shapes at a Mach Number of 1.62 With and Without Fins
Wind-tunnel investigation of the vortex wake and downwash field behind triangular wings and wing-body combinations at supersonic speeds
Weight Bar Charts
Tests in the Ames 40- by 80-foot wind tunnel of an airplane configuration with a variable-incidence triangular wing and an all-movable horizontal tail
The Effect of Canopy Location on the Aerodynamic Characteristics of a Sweptback Wing-Body Configuration at Transonic Speeds
Pressure distributions on triangular and rectangular wings to high angles of attack Mach numbers 1.45 and 1.97
Theory and Procedure for Determining Loads and Motions in Chine-Immersed Hydrodynamic Impacts of Prismatic Bodies
Flight-Test Evaluation of the Longitudinal Stability and Control Characteristics of 0.5-Scale Models of the Fairchild Lark Pilotless-Aircraft Configuration: Standard Configuration with Wing Flaps Deflected 60 Degrees and Model having Tail in Line with Wings, TED No. NACA 2387
Investigation of the Low-Speed Stability and Control Characteristics of a 1/7-Scale Model of the North American X-15 Airplane
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