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National Advisory Committee for Aeronautics Collection
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Longitudinal Characteristics at Transonic and Supersonic Speeds of a Rocket-Propelled Airplane Model Having a 60-Degree Delta Wing and Low Swept Horizontal Tail
Transonic Wind-Tunnel Investigation of the Aerodynamic Loading Characteristics of a 60 Degree Delta Wing in the Presence of a Body With and Without Indentation
Sea-level static equilibrium performance of actual two-spool turbojet engine and comparison with hypothetical engine
The Origin and Distribution of Supersonic Store Interference From Measurement of Individual Forces on Several Wing-Fuselage-Store Configurations 3 - Swept-Wing Fighter-Bomber Configuration With Large and Small Stores. Mach Number, 1.61
Performance of an Isentropic, All-Internal-Contraction, Axisymmetric Inlet Designed for Mach 2.50
Design and Experimental Investigation of a Single-Stage Turbine With a Rotor Entering Relative Mach Number of 2
Experimental Investigation of Various Wing-Mounted External Stores on a Wing-Fuselage Combination Having a Sweptback Wing of Inverse Taper Ratio
Flow studies in the asymmetric adjustable nozzle of the Ames 6-by 6-foot supersonic wind tunnel
Reynolds number effect on axial-flow compressor performance
A comparison of two submerged inlets at subsonic and transonic speeds
Investigation of a Shrouded and an Unshrouded Axial-Flow Supersonic Compressor
An Investigation at Subsonic Speeds of the Rolling Effectiveness of a Small Perforated Spoiler on a Wing Having 45 Degrees of Sweepback
The effect of various aerodynamic balances on the low-speed lateral-control and hinge-moment characteristics of a 0.20-chord partial-span outboard aileron on a wing with leading edge swept back 51.3 degrees
The longitudinal characteristics at Mach numbers up to 0.92 of a cambered and twisted wing having 40 degrees of sweepback and an aspect ratio of 10
Investigation of an NACA Submerged Inlet at Mach Numbers from 1.17 to 1.99
Initial flight investigation of a twin engine supersonic ram jet
The origin and distribution of supersonic store interference from measurement of individual forces on several wing-fuselage-store configurations 3: swept-wing fighter-bomber configuration with large and small stores. Mach number 1.61
Some Features of Artificially Thickened Fully Developed Turbulent Boundary Layers with Zero Pressure Gradient
Note on Hovering Turns with Tandem Helicopters
A method for simulating the atmospheric entry of long-range ballistic missiles
A study of air flow in an engine cylinder
Wind-tunnel investigation of the low-speed aerodynamic characteristics of a hypersonic glider configuration
The static and dynamic-rotary stability derivatives at subsonic speeds of a model of the X-15 research airplane
Theory of wing-body drag at supersonic speeds
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