Injection into a supersonic stream from the windward side of sweptback injectors at angle of attack
Windward injection into supersonic stream at angle of attack, minimizing vortex disruption
Hersch, M.↗
Engineering topics
Hersch, M.
Publications and source records attributed to Hersch, M..
Jet penetration into Mach 2 airstream using sweptback injectors at angle of attack
Jet penetration into Mach 2 airstream using sweptback injectors at angle of attack
Hersch, M.↗
Effect of interacting vortices on jet penetration into a supersonic stream
Interacting vortices effects on jet penetration into supersonic streams
Hersch, M.↗
Supersonic jet penetration /up to Mach 4/ into a Mach 2 airstream
Helium injection Mach number effect on supersonic jet penetration into Mach 2 air stream from flat plate determined from concentration measurements
Hersch, M.↗
A schlieren technique for measuring jet penetration into a supersonic stream
Schlieren optical method for measuring He jet penetration into supersonic flow
Hersch, M.↗
Optical study of sonic and supersonic jet penetration from a flat plate into a Mach 2 airstream
Optical study of sonic and supersonic jet penetration from flat plate into Mach 2 airstream
Hersch, M.↗
Supersonic jet penetration /up to Mach 4/ into a Mach 2 airstream
Helium injection Mach number effect on supersonic jet penetration into Mach 2 air stream from flat plate determined from concentration measurements
Hersch, M.↗
Effect of angle of attack and injection pressure on jet penetration and spreading from a delta wing in supersonic flow
Effect of angle of attack and injection pressure on jet penetration and spreading from delta wing in supersonic flow
Hersch, M.↗
Vortex enhancement of jet penetration in supersonic flow.
Vortex motion enhancement of jet penetration and spreading in supersonic fuel injection into large diameter combustors
Hersch, M.↗
Performance and stability characteristics of nitrogen tetroxide-hydrazine combustors
Small uncooled combustion chamber tests of performance and stability characteristics of nitrogen tetroxide-hydrazine propellant
Hersch, M.↗
Hydrogen-oxygen chemical reaction kinetics in rocket engine combustion
Hydrogen-oxygen chemical reaction kinetics in rocket engine combustion
Hersch, M.↗
Gaseous-hydrogen liquid-oxygen rocket combustion at supercritical chamber pressures
Chamber pressure variations and rocket combustor performance for gaseous hydrogen-liquid oxygen propellant system
CHAMBER PRESSURE↗
A mixing model for rocket engine combustion
Model for prediction of rocket engine combustion with performance parameters of gas phase turbulent diffusion, and mixing of oxidizer and fuel vapors
ROCKET ENGINE↗