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Title
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STOL High-Lift Design Study Volume I. State-of-the-Art Review of STOL Aerodynamic Technology
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Date
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1971
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Index Abstract
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Not Available
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Photo Quality
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Not Needed
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Report Number
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AFFDL TR 71-26 Volume I
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Creator
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May, Fred
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Widdison, Coli A.
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Corporate Author
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Boeing Company
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Laboratory
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Air Force Flight Dynamics Laboratory
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Extent
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204
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Identifier
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AD0724185
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Access Rights
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This document has been approved for public release and sale; its distribution is unlimited.
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Distribution Classification
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1
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Contract
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F33615-70-C-1277
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DoD Project
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None Given
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DoD Task
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None Given
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DTIC Record Exists
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Yes
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Distribution Change Authority Correspondence
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None
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Distribution Conflict
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No
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Abstract
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The state of the art of STOL aerodynamic technology for selected lift/propulsion concepts has been surveyed to identify the available test data and prediction methods in the literature. The report consists of two volumes. In Volume I important areas of technology and information necessary for the evaluation of STOL aircraft aerodynamics are listed; the aerodynamic test data and prediction methodology relevant to the deflected slipstream and externally blown flap concepts are assessed, with emphasis on the latter; an empirical method for the prediction of the longitudinal aerodynamic characteristics of externally blown flap configurations is presented; and high-lift technology for five lift/propulsion concepts is assessed in application to a medium-sized STOL transport. Volume II consists of a bibliography that resulted from a literature search for aerodynamic information related to seven lift/propulsion concepts suitable for STOL aircraft. The bibliography contains references to approximately 900 reports classified by concept and by technological area.
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Report Availability
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Full text available
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Date Issued
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1971-04
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Provenance
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Bombardier/Aero
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Type
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report
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Format
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1 online resource
