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There are a total of 35 record(s) matching your query.
Sorted by: Date Added To NTRS in Descending order
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Turbulent Friction in the Boundary Layer of a Flat Plate in a Two-Dimensional Compressible Flow at High Speeds
Author(s): Frankl, F.; Voishel, V.
Abstract: In the present report an investigation is made on a flat plate in a two-dimensional compressible flow of the effect of compressibility and heating on the turbulent frictional drag coefficient in the boundary layer of an ...
NASA Center: NACA (Unspecified Center)
Publication Year: 1943
Added to NTRS: 2005-09-21
Document ID: 20050029417; Report Number: NACA-TM-1053
Aerodynamic Characteristics of Four Republic Airfoil Sections from Tests in Langley Two-Dimensional Low-Turbulence Tunnels
Author(s): Klein, Milton M.
Abstract: Four airfoils sections, designed by the Republic Aviation Corporation for the root and tip sections of the XF-12 airplane, were tested in the Langley two-dimensional low-turbulence tunnels to obtain their aerodynamic ...
NASA Center: Langley Research Center, NACA (Unspecified Center)
Publication Year: 1945
Added to NTRS: 2005-08-25
Document ID: 20050185542; Report Number: NACA-MR-L5I19
Wind-Tunnel Tests of a 1/6-Scale Model of Republic XF-12 Vertical Tail with Stub Fuselage and Stub Horizontal Tail
Author(s): MacLachlan, Robert
Abstract: A 1/6-scale model of the Republic XF-12 vertical tail with stub fuselage and stub horizontal tail was tested in the Langley stability tunnel to determine the aerodynamic characteristics of the model, The investigation ...
NASA Center: Langley Research Center, NACA (Unspecified Center)
Publication Year: 1945
Added to NTRS: 2005-08-25
Document ID: 20050185538; Report Number: NACA-MR-L5E21
Wind-Tunnel Measurements on the Wing of the Henschel Missile "Zitterrochen" in Subsonic and Supersonic Velocities
Author(s): Kehl
Abstract: Supplementing the measured results previously reported, this investigation of three-component measurements on a wing model of the missile "ZR 2.0" was conducted in the subsonic wind tunnel (open-jet 215-millimeter diameter) ...
NASA Center: NACA (Unspecified Center)
Publication Year: 1948
Added to NTRS: 2005-08-25
Document ID: 20030067832; Report Number: DLUM-3161
Wind-Tunnel Tests of a 1/6-Scale Model of Republic XF-12 Vertical Tail Incorporating a De-Icing Air Duct
Author(s): MacLachlan, Robert; Miller, Sadie M.
Abstract: A 1/6-scale model of the Republic XF-12 vertical tail with stub fuselage, stub horizontal tail, and a de-icing air duct was tested in the Langley stability tunnel. The investigation consisted of a study of the effects of the ...
NASA Center: Langley Research Center, NACA (Unspecified Center)
Publication Year: 1945
Added to NTRS: 2005-08-25
Document ID: 20050185539; Report Number: NACA-MR-L5G18a
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