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NASA MEMO 6-5-59 REV A-1959 Wind-Tunnel Investigation at Subsoni


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Standard Title: Wind-Tunnel Investigation at Subsonic and Supersonic Speeds of the Static and Dynamic Stability Derivatives of an Airplane Model with an Unswept Wing and a High Horizontal Tail
Standard NO.:NASA MEMO 6-5-59 REV A-1959
Papges: 80

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This product was added to our catalog on Saturday 09 July, 2016.