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National Advisory Committee for Aeronautics Collection
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National Advisory Committee for Aeronautics Collection
222
Technical Report Archive and Image Library
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NACA Research Memorandums
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NACA Research Memorandums
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Aerodynamic characteristics and pressure distributions of a 6-percent-thick 49 degree sweptback wing with blowing over half-span and full-span flaps
Aerodynamic Characteristics Including Scale Effect of Several Wings and Bodies Alone and in Combination at a Mach Number of 1.53
Aerodynamic characteristics of a wing with quarter-chord line swept back 45 degrees, aspect ratio 6, taper ratio 0.6, and NACA 65A009 airfoil section
Aerodynamic characteristics of NACA RM-10 missile in 8- by 6-foot supersonic wind tunnel at Mach numbers from 1.49 to 1.98 1: presentation and analysis of pressure measurements (stabilizing fins removed)
Aerodynamic control of supersonic inlets for optimum performance
Aerodynamic Load Distribution on a 45 Degree Sweptback Wing With Leading-Edge Chord-Extensions at Transonic Speeds, Including Effects of a Spoiler-Slot-Deflector Aileron
Air Force Tests of Sperry Messenger Model With Six Sets of Wings
Altitude Performance of a Turbojet Engine Using Pentaborane Fuel
Altitude performance of a turbojet engine using pentaborane fuel
Altitude-Wind-Tunnel Investigation of the 19B-2, 19B-8, and 19XB-1 Jet-Propulsion Engines 2 - Analysis of Turbine Performance of the 19B-8 Engine
Analysis and modification of theory for impact of seaplanes on water
Analysis of performance of four symmetrical-diagram-type subsonic inlet-stage axial-flow compressors
Analytical comparison of turbine-blade cooling systems designed for a turbojet engine operating at supersonic speed and high altitude 1: liquid-cooling systems
Approximate Stress Analysis of Multistringer Beams With Shear Deformation of the Flanges
Blowing Over the Flaps and Wing Leading Edge of a Thin 49 Degree Swept Wing-Body-Tail Configuration in Combination With Leading-Edge Devices
Calculated condenser performance for a steam turbine power plant for aircraft
Canard Hinge Moments and Longitudinal Stability of a 1/7-Scale Model of the Convair B-58 External Store in a Free-Flight Investigation at Mach Numbers From 0.94 to 2.58
Canard Hinge Moments and Longitudinal Stability of a 1/7-Scale Model of the Convair B-58 External Store in a Free-Flight Investigation at Mach Numbers From 0.94 to 2.58: Coord. No. AF-204
The characteristics of 78 related airfoil sections from tests in the variable-density wind tunnel
Coking of JP-4 fuels in electrically heated metal tubes
Comparison Between Analytical and Wind-Tunnel Results on Flutter of Several Low-Aspect-Ratio, High-Density, Unswept Wings at High Subsonic Speeds and Zero Angle of Attack
Comparison of Measured Efficiencies of Nine Turbine Designs with Efficiencies Predicted by Two Empirical Methods
Component Performance Investigation of J71 Type II Turbines 3 - Overall Performance of J71 Type IIA Turbine
Compressible-Flow Solutions for the Actuator Disk
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