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Calculation Of Sidewall Boundary Layer Parameters From Rake Measurements For The Langley 0.3 Meter Transonic Cryogenic Tunnel by A. V. Murthy

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1NASA Technical Reports Server (NTRS) 19870007374: Calculation Of Sidewall Boundary-layer Parameters From Rake Measurements For The Langley 0.3-meter Transonic Cryogenic Tunnel

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Correction of airfoil data for sidewall boundary-layer effects requires a knowledge of the boundary-layer displacement thickness and the shape factor with the tunnel empty. To facilitate calculation of these quantities under various test conditions for the Langley 0.3 m Transonic Cryogenic Tunnel, a computer program was written. This program reads the various tunnel parameters and the boundary-layer rake total head pressure measurements directly from the Engineering Unit tapes to calculate the required sidewall boundary-layer parameters. Details of the method along with the results for a sample case are presented.

“NASA Technical Reports Server (NTRS) 19870007374: Calculation Of Sidewall Boundary-layer Parameters From Rake Measurements For The Langley 0.3-meter Transonic Cryogenic Tunnel” Metadata:

  • Title: ➤  NASA Technical Reports Server (NTRS) 19870007374: Calculation Of Sidewall Boundary-layer Parameters From Rake Measurements For The Langley 0.3-meter Transonic Cryogenic Tunnel
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  • Language: English

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