TIME REQUIRED FOR ESTABLISHING DETACHED BOW SHOCK.

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Abstract:

The trajectory of the detached bow shock subsequent to the impulsive start of a flat nosed circular cylinder in an ideal gas is determined on the hypotheses that the shock is plane over the projection of the face of the body the mean value of the mass flux across the upstream projection to the shock of the lateral surface is independent of time and the local fluid density between the shock and body does not vary with time. Author

Author(s):
Miles, J. W. ; Mirels, H. ; Wang, H. E.
Author Organization(s):
AEROSPACE CORP EL SEGUNDO CA LAB OPERATIONS
Descriptive Note:
Technical documentary rept.,
Annotation:
Time required for establishing detached bow shock.
Pagination:
0008

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
TDR-669(6240-10)-3, SSD-TR-66-29
Contract/Grant Number(s):
AF 04(695)-669
Monitor Series:
TR-66-29
 Subject Terms
Communities of Interest:
Air Platforms
Descriptor(s):
(*SHOCK WAVES, TRAJECTORIES), BLUNT BODIES, CYLINDRICAL BODIES, SUPERSONIC FLOW, CONTROL SURFACES, GAS FLOW, HYPERSONIC FLOW, DENSITY, TIME, COMPRESSIBLE FLOW, MATHEMATICAL ANALYSIS
Field(s)/Group(s):
Fluid Mechanics
Keyword(s):
BOW SHOCK
Report Date:
1965 Jan 01