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

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

著者名:

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

掲載資料名:

NASA Technical Reports

発行年:

1991

号:

NASA-CR-184141

通号:

G3/20 0008211

パート:

NAS 1.26:184141

ペーパー番号:

N91-21239

開始ページ:

1

終了ページ:

126

総ページ数:

126

出版情報:

National Aeronautics and Space Adminstration

言語:

英語

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00001427
論文注記:	NAS8-37682

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