41 pages matching Langley Research Center in this book
Results 1-3 of 41
What people are saying - Write a review
We haven't found any reviews in the usual places.
AIAA Airstream boundary-layer thickness Cl Cl Cl Cl pi CM CM equation figure 13 flat-plate flow contours fM pg free-stream hydrogen flow rate hydrogen mass fraction I I I I I I I injection of hydrogen injection station injector jet diameter 6/D Langley Research Center Mach number Marvin G mass flow mass-weighted total pressure maximum concentration maximum hydrogen concentration mixing rate mixing region mole fraction NASA TN Nondimensional parameters percent pg CM pg pg fM pg pg pg pi Cl point of maximum Povinelli presented in figure pressure recovery profile shape ratio of boundary-layer Scramjet SSVH Supersonic Stream thickness to jet total-pressure losses total-pressure profiles total-pressure recovery turbulent boundary layer UI Ui Ui UJ UJ Ui UJ UJ UJ Ul UJ unit area vertical