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Wind tunnel investigationof the static and dynamicrotary stability derivativesofa fllat top wing body model at mach numbers of 2.5, 3.0 and 3.5 [NASA TM X-361]

By: Lampkin, Bedford A.
Contributor(s): Endicott, Kenneth C.
Material type: materialTypeLabelBookSeries: National Aeronautics and Space Administration. Publisher: Washington, D. C. National Aeronautics and Space Administration 1960Description: 41p.Subject(s): Wind -- Tunnel
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Item type Current location Collection Call number Status Date due Barcode Item holds
Reference Reference PK Kelkar Library, IIT Kanpur
COMPACT STORAGE (BASEMENT) Not for loan 102421 [X-361]
Total holds: 0

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