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National Advisory Committee for Aeronautics Collection
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National Advisory Committee for Aeronautics Collection
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Technical Report Archive and Image Library
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NACA Research Memorandums
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NACA Technical Reports
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NACA Research Memorandums
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Aircraft Power-Plant Instruments
Analysis of Jet-Propulsion-Engine Combustion-Chamber Pressure Losses
Application of blade cooling to gas turbines
Combined Effects of Wing Taper and Low Horizontal-Tail Position on Longitudinal Stability of a 45 Degree Sweptback Wing-Body Combination at Transonic Speeds
Correlation by the Hypersonic Similarity Rule of the Pressure Distributions and Wave Drags for Minimum-Drag Nose Shapes at Zero Angle of Attack
Correlation of cylinder-head temperatures and coolant heat rejections of a multicylinder, liquid-cooled engine of 1710-cubic-inch displacement
Development of Outboard Nacelle for the XB-36 Airplane
Effect of Increase in Angle of Dead Rise on the Hydrodynamic Qualities of a Seaplane Configuration Incorporating High Wing Loading
Effect of inlet oxygen concentration on combustion efficiency of J33 single combustor operating with gaseous propane
Effect of Nose Shape and Wing Thickness Ratio on the Drag at Zero Lift of a Missile Having Triangular Wings and Tails
Effect of wing sweep, taper, and thickness ratio on the transonic drag characteristics of wing-body combinations
The effects of fences on the high-speed longitudinal stability of a swept-wing airplane
The effects of various parameters including Mach number on propeller blade flutter with emphasis on stall flutter
An experimental investigation at Mach numbers from 2.1 to 3.0 of circular-internal-contraction inlets with translating centerbodies
Experimental Investigation of Flutter and Divergence Characteristics of the Rocket-Motor Fin of the ASROC Missile
Experimental investigation of flutter and divergence characteristics of the rocket-motor fin of the ASROC missile: COORD. No. N-AM-66
Experimental investigation of the effectiveness of various suction-slot arrangements as a means for increasing the maximum lift of the NACA 65(sub 3)-018 airfoil section
Experimental Investigation of the Effects of Sweepback on the Flutter of a Uniform Cantilever Wing With a Variably Located Concentrated Mass
Experimental investigation of the effects of viscosity on the drag and base pressure of bodies of revolution at a Mach number 1.5
Factors That Affect Operational Reliability of Turbojet Engines
Flight Determination of the Lateral Handling Qualities of the Bell X-5 Research Airplane at 58.7 Degrees Sweepback
Flight Investigation at High-Subsonic, Transonic, and Supersonic Speeds to Determine Zero-Lift Drag of Bodies of Revolution Having Fineness Ratio of 6.04 and Varying Positions of Maximum Diameter
Flight Investigation of the Effects of Ice on an I-16 Jet-Propulsion Engine
Flutter Investigation on the High Subsonic and Transonic Speed Range on Cantilever Delta-Wing Plan Forms With Leading-Edge Sweepback of 60 Degrees, 53 Degrees 8', and 45 Degrees
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