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Wind Tunnel Force And Flow Visualization Data At Mach Numbers From 1.6 To 4.63 For A Series Of Bodies Of Revolution At Angles Of Attack From 4 ̊to 60 ̊ by Emma Jean Landrum

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1NASA Technical Reports Server (NTRS) 19790013871: Wind-tunnel Force And Flow Visualization Data At Mach Numbers From 1.6 To 4.63 For A Series Of Bodies Of Revolution At Angles Of Attack From Minus 4 Deg To 60 Deg

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Flow visualization and force data for a series of six bodies of revolution are presented without analysis. The data were obtained in the Langley Unitary Plan wind tunnel for angles of attack from -4 deg to 60 deg. The Reynolds number used for these tests was 6,600,000 per meter.

“NASA Technical Reports Server (NTRS) 19790013871: Wind-tunnel Force And Flow Visualization Data At Mach Numbers From 1.6 To 4.63 For A Series Of Bodies Of Revolution At Angles Of Attack From Minus 4 Deg To 60 Deg” Metadata:

  • Title: ➤  NASA Technical Reports Server (NTRS) 19790013871: Wind-tunnel Force And Flow Visualization Data At Mach Numbers From 1.6 To 4.63 For A Series Of Bodies Of Revolution At Angles Of Attack From Minus 4 Deg To 60 Deg
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  • Language: English

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