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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 Research Memorandums
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National Advisory Committee for Aeronautics Collection
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Wind Tunnel Investigation at High Subsonic Speeds of Drag at 0 Degrees Angle of Attack of Swept-Wing Fuselage Models With Pylon Mounted and Semisubmerged Missiles
Synthesis and Hydrolysis-Rate Studies of Decaborane Derivatives
Estimation of Range of Stability Derivatives for Current and Future Pilotless Aircraft
Some preliminary results in the determination of aerodynamic derivatives of control surfaces in the transonic speed range by means of a flush-type electrical pressure cell
Flight and Test-Stand Investigation of High-Performance Fuels in Pratt & Whitney R-1830-94 Engines 4: Comparison of Cooling Characteristics of Flight and Test-Stand Engines
Free-flight measurements at Mach numbers from 0.7 to 1.6 of some effects of airfoil-thickness distribution and trailing-edge angle on aileron rolling effectiveness and drag for wings with 0 and 45 degrees sweepback
Some Effects of Fuselage Interference, Wing Interference, and Sweepback on the Damping in Roll of Untapered Wings as Determined by Techniques Employing Rocket-Propelled Vehicles
Investigation of Turbine of Mark 25 Torpedo Power Plant with Five Nozzle Designs
Elastic Buckling Under Combined Stresses of Flat Plates With Integral Waffle-Like Stiffening
Investigation of the NACA 4-(5)(05)-037 six- and eight-blade, dual-rotation propellers at positive and negative thrust at Mach numbers up to 0.90, including some aerodynamic characteristics of the NACA 4-(5)(05)-041 two- and four-blade, single-rotat
Damping in Roll of Rocket-Powered Test Vehicles Having Swept, Tapered Wings of Low Aspect Ratio
Derivation of the Equations of Motion of a Symmetrical Wing-Tip-Coupled Airplane Configuration With Rotational Freedom at the Junctures
Theoretical Calculations of the Stability Derivatives at Supersonic Speeds for a High-Speed Airplane Configuration
An analytical study of sideslip angles and vertical-tail loads in rolling pullouts as affected by some characteristics of modern high-speed airplane configurations
Analysis of Wind-Tunnel Tests at Low Speeds of a Four-Engine Propeller-Driven Airplane Configuration Having a Wing With 40 Degrees of Sweepback
Performance of Inconel 739 Buckets in J33-9 Turbojet Engine
Analysis of turbojet-engine controls for afterburning starting
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
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
Structural Design and Engine Evaluation of an Air-Cooled Turbine Blade Composed of Corrugation and a Semistrut for Operation at a Tip Speed of 1200 Feet Per Second
Experimental Investigation of Several Water-Injection Configurations for Turbine-Blade Spray Cooling in a Turbojet Engine
Comparison of full-scale propellers having R.A.F.-6 and Clark Y airfoil sections
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