SOLID ROCKET BOOSTER INTERNAL FLOW ANALYSIS BY HIGHLY ACCURATE ADAPTIVE COMPUTATIONAL METHODS

SOLID ROCKET BOOSTER INTERNAL FLOW ANALYSIS BY HIGHLY ACCURATE ADAPTIVE COMPUTATIONAL METHODS

Author(s):

Huang, C.Y. ( NATIONAK AERONAUTICS AND SPACE ADMINISTRATION )

Publication title:

NASA Technical Reports

Pub. Year:

1991

Issue:

NASA-CR-184141

No.:

G3/20 0008211

Pt.:

NAS 1.26:184141

Paper no.:

N91-21239

Page(from):

1

Page(to):

126

Pages:

126

Pub. info.:

National Aeronautics and Space Adminstration

Language:

English

Type:

Technical Paper

Details

TDL ID:	ZA00001427
Note for article:	NAS8-37682

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