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NACA Research Memorandums
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Hydrodynamic Characteristics of Missiles Launched Under Water
Analysis of turbojet and ram-jet engine cycles using various fuels
An Investigation of Loads on Ailerons at Transonic Speeds
An Experimental Investigation of the Flow Phenomena Over Bodies at High Angles of Attack at a Mach Number of 2.01
Statistical measurements of landing contact conditions of the Boeing B-47 airplane
Simplified procedures for estimating flap-control loads at supersonic speeds
The Unsteady Normal-Force Characteristics of Selected NACA Profiles at High Subsonic Mach Numbers
Wind-Tunnel Investigation of the Static Longitudinal and Lateral Stability of the Bell X-1A at Supersonic Speeds
Investigation of a Three-Stage Transonic Research Axial-Flow Compressor: Aerodynamic Design and Overall Performance
A Theoretical Analysis of a Simple Aerodynamic Device to Improve the Longitudinal Damping of a Cruciform Missile Configuration at Supersonic Speeds
Flight measurements of the vertical-tail loads on the Convair XF-92A delta-wing airplane
Aerodynamic principles for the design of jet-engine induction systems
Some Recent Experimental Data on Three-Dimensional Oscillating Air Forces
Performance characteristics of hemispherical target-type thrust reversers
The Effect of Wing Profile on the Transonic Characteristics of Rectangular and Triangular Wings Having Aspect Ratios of 3: Transonic Bump Technique
Low-Speed Measurements of Rolling and Yawing Stability Derivatives of a 60 Degree Delta-Wing Model
Altitude performance of compressor, combustor, and turbine components of XT38-A-2 turboprop engine
Zero-Lift Drag of the Chance Vought Regulus II Missile at Mach Numbers Between 0.8 and 2.2 as Determined From the Flight Tests of Two 0.12-Scale Models: TED No. NACA AD 398
Performance of a 16-inch ram-jet engine with a can-type combustor at Mach numbers of 1.50 to 2.16
Effect of rotation of a NACA 1-series E-type cowling on the internal flow and force characteristics of the cowling at Mach numbers up to 0.84 and at an angle of attack of 0 degrees
Experimental Investigation at High Subsonic Speeds to Determine the Rolling-Stability Derivatives of Three Wing-Fuselage Configurations
Longitudinal Stability Characteristics in Accelerated Maneuvers at Subsonic and Transonic Speeds of the Douglas D-558-II Research Airplane Equipped with a Leading-Edge Wing Chord-Extension
Effects of Wing-Fuselage Flow Fields on Missile Loads at Subsonic Speeds
Comparison of Experimental and Theoretical Zero-Lift Wave-Drag Results for Various Wing-Body-Tail Combinations at Mach Numbers Up to 1.9
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