CFD Investigation of Canard-Controlled Missile with Planar and Grid Fins in Supersonic Flow
- 著者名:
- 掲載資料名:
- A collection of technical papers, AIAA Atmospheric Flight Mechanics Conference, Monterey, California, 5-8 August 2002
- シリーズ名:
- AIAA Paper : AIAA Atmospheric Flight Mechanics Conference
- シリーズ巻号:
- 2002
- 発行年:
- 2002
- 巻:
- v. 1
- 通号:
- 2002-4509
- ペーパー番号:
- AIAA-2002-4509
- 開始ページ:
- 429
- 終了ページ:
- 439
- 総ページ数:
- 11
- 出版情報:
- Reston, VA: American Institute of Aeronautics and Astronautics
- ISBN:
- 9781563475474 [1563475472]
- 言語:
- 英語
- 請求記号:
- A07400/024400 (v.1)
- 資料種別:
- テクニカルペーパー
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4
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Deflectable Nose and Canard Controls for a Fin-Stabilized Projectile at Supersonic and Hypersonic Speeds
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WIND-TUNNEL INVESTIGATION AT SUPERSONIC SPEEDS OF A REMOTE-CONTROLLED CANARD MISSILE WITH A FREE-ROLLING-TAIL
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