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871201s1964 ohua bt f000 0 eng d |
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‡a(MiU)99187625985406381
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‡asdr-miu.99187625985406381
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‡a(OCoLC)1109471149
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‡aMAIN
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‡aD 301.45/34-2:63-4179 Part II
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‡aKaufman, Louis G.,
‡eauthor.
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‡aPressure measurements for mach five flows over winged re-entry configurations with aerodynamic controls.
‡nPart II.
‡pConical cabin configuration /
‡cLouis G. Kaufman.
|
264 |
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‡aWright-Patterson Air Force Base, Ohio :
‡bAir Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force,
‡c1964.
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‡avi, 203 pages :
‡billustrations, figures, tables ;
‡c28 cm.
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‡atext
‡btxt
‡2rdacontent
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‡aunmediated
‡bn
‡2rdamedia
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‡avolume
‡bnc
‡2rdacarrier
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‡aTechnical documentary report (Air Force Flight Dynamics Laboratory (U.S.)) ;
‡vAFFDL-RTD-TDR-63-4179, Part II
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‡a"February 1964."
|
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‡aIncludes bibliograpical references (page 5).
|
536 |
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‡aAir Force Contract No.
‡bAF 33(616)-8130, Project No. 8219, Task No. 821902.
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‡aMode of access: Internet.
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‡aHeat
‡xTransmission.
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‡aAirplanes
‡xWings, Swept-back.
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‡aUnited States.
‡bAir Force.
‡bSystems Command,
‡eissuing body.
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‡aAir Force Flight Dynamics Laboratory (U.S.),
‡esponsor.
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‡aGrumman Aircraft Engineering Corporation,
‡esponsor.
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730 |
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‡aTechnical Report Archive & Image Library (TRAIL)
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899 |
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‡a39015104956746
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‡a102892564
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‡b2024-08-06T17:32:14Z
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‡tUS fed doc
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