To Investigate the Effect of Reynolds number, Oscillation rate, Thickness Ratio and Pivot point position on Dynamic stall of an Oscillating Airfoil Hussein Raza Hamdani CAEG-53 (A)
Publisher: Risalpur NUST 2001Edition: 1stDescription: 98pDDC classification: PR-516| Item type | Current location | Home library | Collection | Call number | Status | Date due | Barcode | Item holds |
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Book
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College of Aeronautical Engineering (CAE) | College of Aeronautical Engineering (CAE) | NFIC | PR-516 (Browse shelf) | Available | CAEPR-516 |
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