Engineering topics
Publications and source records attributed to Summerfield, M..
Ignition pressure transient of rocket motor, discussing initial ignition event, flame spreading and final chamber filling, convective heating effect on burning rate, etc
Ignition analysis of condensed phase fuel suddenly exposed to stationary hot oxidizing gas, noting strong pressure effect due to feedback mechanism
Microscopic temperature profiles through propagating solid propellant flames in composite and double base propellants measured, using fine thermocouples
Ignition characteristics of evaporating fuel evaluated by similarity theory and mathematical model analysis
NASA sponsored research in astrophysics and aerospace propulsion and NASA support of graduate education in space sciences and astronautics at Princeton University
Research on mechanism of ignition of solid rocket propellants
Explore the source record for details and available documents.