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NotificationsNotify me of updates to Charts of Pressure Rise Obtainable with Airfoil-Type Axial-Flow

Charts of Pressure Rise Obtainable with Airfoil-Type Axial-Flow
[NACA-TN-1199]
$7.70

(Tech/propulsion/fan:NACA-TN-1199) Kahane, A.: Charts of Pressure Rise Obtainable with Airfoil-Type Axial-Flow Cooling Fans. NACA, Technical Notes. Janury 16, 1946. 55 pages. Paper master; price based on paper copy; see Options below for binding. Price: $7.70

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This product was added to our catalog on Saturday 23 October, 2010.
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