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Large-scale low-speed wind-tunnel tests of a model having a 60 degree delta horizontal canard control surface and wing to obtain static-longitudinal-stability and canard surface hinge-moment data
Aerodynamic Characteristics of a 45 Degree Swept Wing Fighter Airplane Model and Aerodynamic Loads on Adjacent Stores and Missiles at Mach Numbers of 1.57, 1.87, 2.16, and 2.53
Hydrodynamic Characteristics of Missiles Launched Under Water
Estimation of Incremental Pitching Moments Due to Trailing-Edge Flaps on Swept and Triangular Wings
Removal of secondary-flow accumulations in a two-dimensional turbine nozzle passage by boundary-layer bleed
Experimental Flutter Results for Cantilever-Wing Models at Mach Numbers Up to 3.0
Lateral Stability and Control Measurements of a Fighter-Type Airplane With a Low-Aspect-Ratio Unswept Wing and a Tee-Tail
A Bibliography of NACA Reports on Control of Turbojet Engines
Experimental Drag Coefficients of Round Noses With Conical Windshields at Mach Number 2.72
Static longitudinal and lateral stability and control characteristics of an 0.065-scale model of the Chance Vought Regulus II missile at Mach numbers of 1.41, 1.61, and 2.01: TED No. NACA AD 398
Some Recent Experimental Data on Three-Dimensional Oscillating Air Forces
Steady-state and surge characteristics of a compressor equipped with variable inlet guide vanes operating in a turbojet engine
Effect of wing flexibility on the damping roll of a notched delta-wing body combination between Mach numbers 0.6 and approximately 2.2 as determined with rocket-propelled models
Low-Amplitude Damping-in-Pitch Characteristics of Tailless Delta-Wing-Body Combinations at Mach Numbers From 0.80 to 1.35 as Obtained With Rocket-Powered Models
Forces and moments on inclined bodies at Mach numbers from 3.0 to 6.3
An Investigation of the Effects of Jet Exhaust and Reynolds Number Upon the Flow Over the Vertical Stabilizer and Rudder of the Douglas D-558-II Research Airplane at Mach Numbers of 1.62, 1.93, and 2.41
Full-Scale Evaluation of Some Flameholder Design Concepts for High-Inlet-Velocity Afterburners
Analytical Investigation of Fuel-Cooled Turbine Blades With Return-Flow Type of Finned Coolant Passages
Cascade Investigation of Cooling Characteristics of a Castfinned Air-Cooled Turbine Blade for Use in a Turboprop Engine
Analyses for Turbojet Thrust Augmentation With Fuel-Rich Afterburning of Hydrogen, Diborane, and Hydrazine
Effects of Wing-Fuselage Flow Fields on Missile Loads at Subsonic Speeds
Investigation of Aerodynamic Characteristics of an Airplane Configuration Having Tail Surfaces Outboard of the Wing Tips at Mach Numbers of 2.30, 2.97, and 3.51
Investigation of High-Angle-of-Attack Performance of a 14 Deg Ramp-Type Inlet in Various Circumferential Body Locations: Mach Number Range 1.5 to 2.0
Low-Speed Roll Effectiveness of a Differentially Deflected Horizontal-Tail Surface on a 42 Degree Swept-Wing Model
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