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Technical Report Archive and Image Library
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Technical Report Archive and Image Library
15
National Advisory Committee for Aeronautics Collection
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NACA Research Memorandums
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NACA Research Memorandums
11
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United States
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1956
15
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1956
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8th
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8th
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Technical Report Archive and Image Library
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1956
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8th
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The Origin and Distribution of Supersonic Store Interference From Measurement of Individual Forces on Several Wing-Fuselagestore Configurations 6. - Swept-Wing Heavy-Bomber Configuration With Stores of Different Sizes and Shapes
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
Determination of vortex paths by series expansion technique with application to cruciform wings
The origin and distribution of supersonic interference from measurement of individual forces on several wing-fuselage-store configurations 6: swept-wing heavy-bomber configuration with stores of different sizes and shapes
A simulation study of a wingless missile
Longitudinal Stability Investigation for a Mach Number Range of 0.8 to 1.7 of an Airplane Configuration With a 45 Degree Swept Wing and a Low Horizontal Tail
Preliminary Free-Flight Study of the Drag and Stability of a Series of Short-Span Missiles at Mach Numbers From 0.9 to 1.3
Wind-Tunnel Investigation at Transonic Speeds of a Jet Control on a 35 Degree Swept Wing: Transonic-Bump Method
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
A free-flight investigation of the effects of a sonic jet on the total-drag and base-pressure coefficients of a boattail body of revolution from Mach number 0.83 to 1.70
Surface Dosimetry and Effective Energy Calculations
Application and Operation of the 325 Building Well Counter
Technical Information for Application of Differential Pressure Transmitters in Pulse Column Bottom Interface Control Systems
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