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Technical Report Archive and Image Library
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Technical Report Archive and Image Library
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National Advisory Committee for Aeronautics Collection
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NACA Research Memorandums
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An Analytical Evaluation of the Effects of an Aerodynamic Modification and of Stability Augmenters on the Pitch Behavior and Probable Pilot Opinion of Two Current Fighter Airplanes
Effects of Wing Sweep, Horizontal-Tail Configuration, and a Ventral Fin on Static Stability Characteristics of a Model With a Wing of Aspect Ratio 3 at Mach Numbers From 2.29 to 4.65
Investigation of the aerodynamic characteristics of a model of a supersonic bomber configuration with a swept and an unswept wing at Mach numbers from 1.79 to 2.67
Operational problems of manned orbital vehicles
Preliminary Aerodynamic Data Pertinent to Manned Satellite Reentry Configurations
A Wind-Tunnel Investigation of the Wing Loads Due to Deflected Inboard Ailerons on a 45 Degree Sweptback Wing at Transonic Speeds
A Wind-Tunnel Investigation of the Wing Loads Due to Deflected Inboard Ailerons on a 45 Degree Sweptback Wing at Transonic Speeds
An analysis of surface pressures and aerodynamic load distribution over the swept wing of the Douglas D-558-II research airplane at Mach numbers from 0.73 to 1.73
Free-Flight Investigation to Determine the Inlet External Drag of Four Inlet Models at Mach Numbers From 1.50 to 3.00
Buffet Tests of an Attack-Airplane Model With Emphasis on Analysis of Data From Wind-Tunnel Tests
Buffet Tests of an Attack-Airplane Model With Emphasis on Analysis of Data From Wind-Tunnel Tests
Tabulated pressure data for a 60 degree delta-wing-body-tail model with a hot jet exhausting from a pylon-mounted nacelle
Free-Flight Determination of Boundary-Layer Transition and Heat Transfer for a Hemisphere-Cylinder at Mach Numbers to 5.6
Performance Comparison at Mach Numbers 1.8 and 2.0 of Full Scale and Quarter Scale Translating-Spike Inlets
Performance of external-internal compression inlet with abrupt internal turning at Mach numbers 3.0 to 2.0
Pressure Drag of Axisymmetric Cowls Having Large Initial Lip Angles at Mach Numbers From 1.90 to 3.88
Simplified Theory for Dynamic Relation of Ramjet Pressures and Fuel Flow
Altitude Starting Tests of a Small Solid Propellant Rocket
Wind-Tunnel Investigation of the Effect of Spin on the Aerodynamic Characteristics of a 60-Millimeter T-24 Mortar Shell With Several Tail-Fin Configurations
Wind-Tunnel Investigation of the Effect of Spin on the Aerodynamic Characteristics of a 60-Millimeter T-24 Mortar Shell With Several Tail-Fin Configurations
Basic performance characteristics of several subsonic-diffuser-bypass-duct combinations for use with supersonic inlets
Cooling performance and structural reliability of a modified corrugated-insert air-cooled turbine blade with an integrally cast shell and base
Flight Performance of a 2.8 KS 8100 Cajun Solid-Propellant Rocket Motor
Investigation of Static Pressures and Boundary-Layer Characteristics on the Forward Parts of Nine Fuselages of Various Cross-Sectional Shapes at M Infinity Equal 2.01
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