Modification of the composite propellant erosive burning model of Lenoir and Robillard
Journal Article
·
· Combust. Flame; (United States)
Commenting on a paper by King, Glick uses King's numerical estimates and an assumption to show that erosive burning models based on additive heat fluxes are invalid and that erosive burning in composite propellants probably stems from wall shear-induced interactions in the condensed phase melt. In his response. King finds fault with Glick's assumption of a 1-dimensional homogeneous picture of solid propellant combustion. While King declines to defend the model of erosive burning, he disagrees with Glick's argument against summing of heat fluxes. (DDA)
- Research Organization:
- Thiokol Corp., Huntsville, AL
- OSTI ID:
- 7226567
- Journal Information:
- Combust. Flame; (United States), Journal Name: Combust. Flame; (United States) Vol. 27:3; ISSN CBFMA
- Country of Publication:
- United States
- Language:
- English
Similar Records
Radiative heating and erosive burn of a solid propellant subject to electrothermal plasma
Surface erosion studies in a plasma-propellant interaction experiment
Modeling of normal and erosive burning rate of a hot double-base homogeneous propellant
Conference
·
Mon Dec 30 23:00:00 EST 1996
·
OSTI ID:428041
Surface erosion studies in a plasma-propellant interaction experiment
Conference
·
Fri Dec 30 23:00:00 EST 1994
·
OSTI ID:42997
Modeling of normal and erosive burning rate of a hot double-base homogeneous propellant
Journal Article
·
Sun Mar 31 23:00:00 EST 1996
· Combustion and Flame
·
OSTI ID:215678