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National Advisory Committee for Aeronautics Collection
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Effect of inlet-air-flow-distortions on steady-state performance of J65-B-3 turbojet engine
Experimental investigation of effect of cooling air on turbine performance of two turbojet engines modified for air-cooling
A flight investigation at transonic speeds and small angles of attack of the aerodynamic characteristics of a model having a 45 degree sweptback wing of aspect ratio 3 with an Naca 64A006 airfoil section
Investigation of Two Short Annular Diffuser Configurations Utilizing Section and Injection as a Means of Boundary-Layer Control
Interaction of a Free Flame Front With a Turbulence Field
Interference effects at Mach 1.9 on a horizontal tail due to trailing shock waves from an axisymmetric body with an exiting jet
Flight Characteristics of a Wingless Rocket- Powered Model With Four Externally Mounted Air-to-Air Missiles at Mach Numbers 0.7 to 1.6
Investigation at Mach Number 1.62 of the Pressure Distribution Over a Rectangular Wing With Symmetrical Circular-Arc Section and 30-Percent-Chord Trailing-Edge Flap
Investigation of Stresses Due to Thermal Gradients in Typical Aircraft Structures
Aerodynamics of slender bodies at Mach number of 3.12 and Reynolds numbers from 2 x 10(exp 6) to 15 x 10(exp 6) 4: aerodynamic characteristics of series of four bodies having near-parabolic noses and cylindrical afterbodies
Aerodynamic Characteristics at Transonic Speeds of a Tapered 45 Degree Sweptback Wing of Aspect Ratio 3 Having a Full-Span Flap Type of Control With Overhang Balance: Transonic-Bump Method
Measurement of heat-transfer and friction coefficients for flow of air in noncircular ducts at high surface temperatures
Correlation of physical properties with molecular structure for some dicyclic hydrocarbons having high thermal-energy release per unit volume -- 2-alkylbiphenyl and the two isomeric 2-alkylbicyclohexyl series
A limited flight investigation of the effect of dynamic vibration absorbers on the response of an airplane structure during buffeting
The Effect of Base Bleed on the Base Pressure, Lift, Drag, and Pitching Moment of a 10-Percent-Thick Blunt-Base Airfoil at a Mach Number of 2.72
Free-flight investigation, including some effects of wing aeroelasticity, of the rolling effectiveness of an all-movable horizontal tail with differential incidence at Mach numbers from 0.6 to 1.5
Static Thrust and Power Characteristics of Six Full-Scale Propellers
Design and experimental investigation of a single-stage turbine with a downstream stator
Tolerable Limits of Oscillatory Accelerations Due to Rolling Motions Experienced by One Pilot During Automatic-Interceptor Flight Tests
Theoretical performance of liquid hydrogen and liquid fluorine as a rocket propellant for a chamber pressure of 600 pounds per square inch absolute
Static Longitudinal and Lateral Stability and Control Data Obtained from Tests of a 1/15-Scale Model of the Goodyear XZP5K Airship, TED No. NACA DE 211
Theoretical Investigation of the Attack Phase of an Automatic Interceptor System at Supersonic Speeds With Particular Attention to Aerodynamic and Dynamic Representation of the Interceptor
Preliminary Investigation of Modifications to Conventional Airplanes to Give Nonstalling and Short-Landing Characteristics
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