Accession Number:
ADA037247
Title:
A Simplified Model of Shock-on-Shock Interaction
Descriptive Note:
Final rept. Feb-30 Sep 1976
Corporate Author:
MARTIN MARIETTA AEROSPACE ORLANDO FL
Personal Author(s):
Report Date:
1976-08-01
Pagination or Media Count:
75.0
Abstract:
A simplified model is presented of the shock-on-shock problem as it pertains to the encounter between a supersonic cone and a planar blast wave. The model provides an accurate and inexpensive means of predicting the circumferential distribution of peak pressures and pulse duration for all encounter angles between nose-on and broadside with the cone at zero or small angles of attack.
Descriptors:
- *BLAST WAVES
- *CONICAL BODIES
- *EXPLOSION EFFECTS
- ANGLE OF ATTACK
- ARRIVAL
- COMPUTERIZED SIMULATION
- DISTRIBUTION
- FLOW SEPARATION
- FRATRICIDE
- HYPERSONIC FLIGHT
- INTERACTIONS
- INTERCEPTORS
- MATHEMATICAL MODELS
- MATHEMATICAL PREDICTION
- OVERPRESSURE
- REENTRY VEHICLES
- SHARP BODIES
- SHOCK WAVES
- SUPERSONIC FLIGHT
- TIME
Subject Categories:
- Explosions