NASA Technical Reports Server (NTRS) 19860014090: Aerodynamic Characteristics of a Supersonic Fighter Aircraft Model at Mach 0.40 to 2.47Report as inadecuate



 NASA Technical Reports Server (NTRS) 19860014090: Aerodynamic Characteristics of a Supersonic Fighter Aircraft Model at Mach 0.40 to 2.47


NASA Technical Reports Server (NTRS) 19860014090: Aerodynamic Characteristics of a Supersonic Fighter Aircraft Model at Mach 0.40 to 2.47 - Download this document for free, or read online. Document in PDF available to download.

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The aerodynamic characteristics of an advanced twin-engine fighter aircraft designed for supersonic cruise have been studied in the Langley 16-Foot Transonic Tunnel and the Lewis 10- by 10-Foot Supersonic Tunnel. The objective of this investigation was to establish an aerodynamic data base for the configuration with flow-through nacelles and repres

Author: NASA Technical Reports Server (NTRS)

Source: https://archive.org/







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