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National Advisory Committee for Aeronautics Collection
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Acceleration Measurements During Landings of a 1/5.5-Size Dynamic Model of the Columbia XJL-1 Amphibian in Smooth Water and in Waves: Langley Tank Model 208M, TED No. NACA 2336
Additional measurements of the low-speed static stability of a configuration employing three triangular wing panels and a body of equal length
Aerodynamic Characteristics at Supersonic Speeds of a Series of Wing-Body Combinations Having Cambered Wings With an Aspect Ratio of 3.5 and a Taper Ratio of 0.2: Effect at M = 2.01 of Nacelle Shape and Position on the Aerodynamic Characteristics in Pitch of Two Wing-Body Combinations with 47 Degree Sweptback Wings
Aerodynamic Characteristics at Transonic Speeds of a Tapered 45 Degree Sweptback Wing of Aspect Ratio 3 Having a Full-Span Flap Type of Control With Overhang Balance: Transonic-Bump Method
Aerodynamic characteristics of a 60 degree delta wing having a half-delta tip control at a Mach number of 4.04
Aerodynamic Characteristics of Missile Configurations With Wings of Low Aspect Ratio for Various Combinations of Forebodies, Afterbodies, and Nose Shapes for Combined Angles of Attack and Sideslip at a Mach Number of 2.01
Aerodynamics of slender bodies at Mach number of 3.12 and Reynolds numbers from 2 x 10(exp 6) to 15 x 10(exp 6) 4: aerodynamic characteristics of series of four bodies having near-parabolic noses and cylindrical afterbodies
Altitude-Wind-Tunnel Investigation of the 19B-2, 19B-8 and 19XB-1 Jet- Propulsion Engines: 4 - Analysis of Compressor Performance
Altitude-wind-tunnel investigations of thrust augmentation of a turbojet engine 1: Performance with tail-pipe burning
The Ames supersonic free-flight wind tunnel
The Ames Supersonic Free-Flight Wind Tunnel
Analysis of cooling-air requirements of corrugated-insert-type turbine blades suitable for a supersonic turbojet engine
Analysis of Factors Affecting Selection and Design of Air-Cooled Single-Stage Turbine for Turbojet Engines 1: Turbine Performance and Engine Weight-Flow Capacity
An analysis of longitudinal-control problems encountered in flight at transonic speeds with a jet-propelled airplane
Analysis of V-G records from ten types of Navy airplanes in squadron operations during the period 1949 to 1953
Analytic evaluation of effect of inlet-air temperature and combustion pressure on combustion performance of boron slurries and blends of pentaborane in octene-1 : Supplement I - Influence of new boric-oxide vapor-pressure data on calculated performanc
Analytical determination of effect of turbine cooling-air-impeller performance on engine performance and comparison of experimentally determined performance of impellers with and without inducer vanes
Analytical investigation of factors affecting the performance of single-stage turbines having rotor-tip discharge of cooling air
Applications of auxiliary air injectors to supersonic wind tunnels
Bodies of Revolution for Minimum Drag at High Supersonic Airspeeds
Calculated and measured pressure distributions over the midspan section of the NACA 4412 airfoil
Characteristics of Four Nose Inlets as Measured at Mach Numbers Between 1.4 and 2.0
Comparative flight performance with an NACA Roots supercharger and a turbocentrifugal supercharger
Comparison of Alcogas Aviation Fuel With Export Aviation Gasoline
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