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NACA Research Memorandums
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Effects of Span and Spanwise and Chordwise Location on the Control Effectiveness of Spoilers on a 50 Degree Sweptback Wing at Mach Numbers of 1.41 and 1.96
The Effect of Magnesium Particles of Various Equivalent Diameters on Some Physical Properties of Petrolatum-Stabilized Magnesium-Hydrocarbon Slurries
Analysis of Wind-Tunnel Tests at Low Speeds of a Four-Engine Propeller-Driven Airplane Configuration Having a Wing With 40 Degrees of Sweepback
Experimental Investigation of a Five-Stage Axial-Flow Research Compressor With Transonic Rotors in All Stages 2: Compressor Over-All Performance
Pumping Characteristics for Several Simulated Variable-Geometry Ejectors With Hot and Cold Primary Flow
An Analysis of the Transonic and Supersonic Performance of Several Fixed-Geometry Air Inlets
An analysis of the transonic and supersonic performance of several fixed-geometry air inlets
Wind-Tunnel Investigation at Transonic Speeds of a Jet Control on a 35 Degree Swept Wing: Transonic-Bump Method
Transportation of liquid fluorine
A survey of unclassified axial-flow-compressor literature
Performance of Inconel 739 Buckets in J33-9 Turbojet Engine
Analysis of turbojet-engine controls for afterburning starting
A Comparison of Flight-Measured Carrier-Approach Speeds With Values Predicted by Several Different Criteria for 41 Fighter-Type Airplane Configurations
Free-Flight Experience of the Lateral Stability Characteristics at Low Lift of a 45 Degree Swept-Wing Rocket-Propelled Model Equipped With a Nonlinear Yaw-Rate Damper System at Mach Numbers From 0.76 to 1.73
An Investigation of the Release Characteristics of a 1/30 Dynamically Scaled AVCO Booster Vehicle from the Simulated Bomb Bay of the B-52 Airplane : COORD. No. AF-AM-59
Synthesis and Hydrolysis-Rate Studies of Decaborane Derivatives
Chemical igniters for starting jet fuel - nitric acid rockets
Performance of Basic XJ79-GE-1 Turbojet Engine and Its Components
A theoretical and experimental study of boric oxide deposition on a surface immersed in an exhaust gas stream from a jet-engine combustor, including a method of calculating deposition rates on surfaces
Preliminary investigation of dynamic lateral stability characteristics of a configuration of the North American X-15 research airplane
Physical and Chemical Properties of HEF-2 (NACA Fuel 56Z4)
Analytical and experimental investigation of the effects of compressor interstage air bleed on performance characteristics of a 13-stage axial-flow compressor
Tests of Aerodynamically Heated Multiweb Wing Structures in a Free Jet at Mach Number 2: Four Aluminum-Alloy Models of 20-Inch Chord and Span With 0.064-Inch-Thick Skin, 0.025-Inch-Thick Ribs and Webs, and Zero, One, Two, or Three Chordwise Ribs
Exploratory Investigation of the Effect of Wing Slots and Leading-Edge Slats on the Longitudinal Stability Characteristics of a 45 Degree Sweptback Wing-Fuselage Configuration
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