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Title
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Methods for Predicting the Aerodynamic and Stability and Control Characteristics of STOL Aircraft. Volume I. Basic Theoretical Methods.
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Date
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1973
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Index Abstract
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Coming Soon
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Photo Quality
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Not Needed
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Report Number
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AFFDL TR 73-146 VOL. I
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Creator
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Goldhammer, M. I.
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Shen, C. C.
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Lopez, M. L.
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Corporate Author
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Douglas Aircraft Company
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Laboratory
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Air Force Flight Dynamics Laboratory
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Extent
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304
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Identifier
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ADA001580
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ADA001580
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Access Rights
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Approved for public release; distribution unlimited.
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Distribution Classification
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1
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Contract
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F33615-71-C-1861
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DoD Project
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643A
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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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Abstract
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The primary goal of the study has been the development of a unified set of analytical methods which would provide the capability to calculate the stability and control characteristics of an arbitrary STOL aircraft configuration that might employ the internally ducted jet flap, externally blown jet flap, or a mechanical high lift system with vectored thrust. This volume presents the complete theoretical development of the relevant analytical methods. In addition, it presents comparisons of these methods with other analytical solutions and with experimental data.
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Report Availability
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Full text available
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Date Issued
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1973-12
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Distribution Conflict
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No
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Date Modified
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Scanned by request 7/1/2020 submitted by Aurora Flight Sciences Corporation (Aerospace Industry - Domestic)
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Provenance
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AFRL/VACA
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Type
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report
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Format
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1 online resource
