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220630s1971 tnua bt f000 0 eng d |
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‡a(MiU)99187626113206381
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‡asdr-miu.99187626113206381
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‡a(OCoLC)1333965260
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‡a(GWLA)gwla on1333965260
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‡aTRAAL
‡beng
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‡cTRAAL
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‡aMAIN
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‡aD 301.45/33:71-077
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‡aBinion, Travis W.,
‡eauthor,
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‡aAn investigation of several slotted wind tunnel wall configurations with a high disk loading V/STOL model /
‡cT.W. Binion, Jr.
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‡aArnold Air Force Base, Tennessee :
‡bArnold Engineering Development Center, Air Force Systems Command, United States Air Force,
‡c1971.
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‡a64 pages :
‡billustrations,
‡c28 cm
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‡atext
‡btxt
‡2rdacontent
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337 |
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‡aunmediated
‡bn
‡2rdamedia
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‡avolume
‡bnc
‡2rdacarrier
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‡aAEDC-TR ;
‡v71-077
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‡aReport was prepared by ARO, Inc., a subsidiary of Sverdrup & Parcel and Associates, Inc.
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‡a"Final Report: November 18 to December 2, 1970."
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‡a"May 1971."
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‡aIncludes bibliographic references (page 22).
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‡aThe investigation reported herein is the experimental portion of a unified theoretical and experimental search for a slotted wind tunnel wall configuration with minimal interference for conventional and V/STOL models. It is shown that theory and experiment are in excellent agreement for the classical case provided an appropriate expression is used to relate the wall geometry to the boundary condition. Classical data correction equations are not appropriate for the V/STOL case, however. An additional term, not predicted by theory, is needed to account for changes in the jet wake. Geometric parameters which influence the wall interference quantities are indicated. Wall configurations are shown which will produce interference-free force data to a jet-to-free-stream velocity ratio of 4.5. (Author).
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‡aMode of access: Internet.
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‡aWind tunnel walls.
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‡aShort take-off and landing aircraft.
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‡aVertically rising aircraft.
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‡aARO, Inc.,
‡esponsor.
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‡aArnold Engineering Development Center,
‡esponsor.
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‡aUnited States.
‡bAir Force.
‡bSystems Command,
‡eissuing body.
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‡aTechnical Report Archive & Image Library (TRAIL)
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‡a39015104952315
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‡a2024-07-29T17:30:02Z
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