The Effects of Body Camber on Body Pressure Distributions and Wing Forces for Mach Numbers from 2.0 to 7.6: Part I: Experimental Data
Item
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Title
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The Effects of Body Camber on Body Pressure Distributions and Wing Forces for Mach Numbers from 2.0 to 7.6: Part I: Experimental Data
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Index Abstract
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Not Available
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Photo Quality
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Incomplete
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Report Number
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ASD TR 61-295 Part I
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Index Price
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$0.00
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Report Availability
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Not available via Contrails
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Creator
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Durgin, F. H.
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Noz, W. C., Jr.
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Date
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1962
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Extent
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83
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Corporate Author
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Massachusetts Institute of Technology Naval Supersonic Facility
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Laboratory
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Flight Control Laboratory
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Contract
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AF 33(616)-7246
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DoD Project
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8219
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DoD Task
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821901
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Distribution Conflict
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No
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Access Rights
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ASTIA
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Distribution Classification
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2
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Abstract
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The abstract for this report is either unavailable or has yet to be entered
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Provenance
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Bombardier/Aero
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Type
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report