NASA Technical Reports Server (NTRS) 19730024451: Calculation procedures for potential and viscous flow solutions for engine inletsReport as inadecuate



 NASA Technical Reports Server (NTRS) 19730024451: Calculation procedures for potential and viscous flow solutions for engine inlets


NASA Technical Reports Server (NTRS) 19730024451: Calculation procedures for potential and viscous flow solutions for engine inlets - Download this document for free, or read online. Document in PDF available to download.

Download or read this book online for free in PDF: NASA Technical Reports Server (NTRS) 19730024451: Calculation procedures for potential and viscous flow solutions for engine inlets
The method and basic elements of computer solutions for both potential flow and viscous flow calculations for engine inlets are described. The procedure is applicable to subsonic conventional (CTOL), short-haul (STOL), and vertical takeoff (VTOL) aircraft engine nacelles operating in a compressible viscous flow. The calculated results compare well

Author: NASA Technical Reports Server (NTRS)

Source: https://archive.org/







Related documents