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NACA Research Memorandums
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Aerodynamic Characteristics of a Number of Modified NACA Four-Digit-Series Airfoil Sections
Aerodynamic characteristics of several flap-type trailing-edge controls on a trapezoidal wing at Mach numbers of 1.61 and 2.01
Aerodynamic Forces and Moments on a Large Ogive-Cylinder Store at Various Locations Below the Fuselage Center Line of a Swept-Wing Bomber Configuration at a Mach Number of 1.61
Aerodynamic heating of aircraft components
Altitude operational characteristics of prototype J40-WE-8 turbojet engine
Analysis of coolant-flow requirements for an improved, internal-strut-supported, air-cooled turbine-rotor blade
Analytical evaluation of effect of equivalence ratio inlet-air temperature and combustion pressure on performance of several possible ram-jet fuels
Application of Radial-Equilibrium Condition to Axial-Flow Turbomachine Design Including Consideration of Change of Entropy With Radius Downstream of Blade Row
Aspects of internal-flow-system design for helicopter propulsive units
Basic pressure measurements on a fuselage and a 45 degrees sweptback wing-fuselage combination at transonic speeds in the slotted test section of the Langley 8-foot high-speed tunnel
Canopy loads investigation for the F6F-3 airplane
Combustion efficiency performance of a MIL-F-5624 type fuel and monomethylnapthalene in a single vaporizing combustor
A comparison of theoretical and experimental loading on a 63 degrees swept-back wing at supersonic speeds
Component performance investigation of J71 experimental turbine 7: effect of first-stator adjustment; over-all performance of J71 turbine with 87-percent-design stator area
Concluding Report on Free-Spinning and Recovery Characteristics of a 1/24-Scale Model of the Grumman F11F-1 Airplane, TED No. NACA AD 395
Control Hinge-Moment and Effectiveness Characteristics of a 60 Degree Half-Delta Tip Control on a 60 Degree Delta Wing at Mach Numbers of 1.41 and 1.96
Data presentation of force characteristics of several engine-strut-body configurations at Mach numbers of 1.8 and 2.0
Description and Investigation of a Dynamic Model of the XH-17 Two-Blade Jet Driven Helicopter
Development of Metal-Bonding Adhesives With Improved Heat-Resistant Properties
Ditching Tests with a 1/16-Size Model of the Navy XP2V-1 Airplane at the Langley Tank No. 2 Monorail
Drag and Longitudinal Trim at Low Lift of the North American YF-100A Airplane at Mach Numbers from 0.76 to 1.77 as Determined from the Flight Test of a 0.11-Scale Rocket Model
Effect at Transonic Speeds of Inboard Spoilers on the Static Longitudinal Stability Characteristics of a 45 Degree Sweptback Wing-Body Combination Having a Leading-Edge Chord-Extension
Effect of boundary-layer control and inlet lip shape on the performance of a twin-scoop air-induction system at Mach numbers from 0 to 1.9
Effect of Large Deflection of a Canard Control and Deflections of a Wing-Tip Control on the Static-Stability and Induced-Roll Characteristics of a Cruciform Canard Missile at a Mach Number of 2.01
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