Pressure measurements for mach five flows over winged re-entry configurations with aerodynamic controls. Part II. Conical cabin configuration

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086 0 ‡aD 301.45/34-2:63-4179 Part II
100 1 ‡aKaufman, Louis G., ‡eauthor.
245 1 0 ‡aPressure measurements for mach five flows over winged re-entry configurations with aerodynamic controls. ‡nPart II. ‡pConical cabin configuration / ‡cLouis G. Kaufman.
264 1 ‡aWright-Patterson Air Force Base, Ohio : ‡bAir Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, ‡c1964.
300 ‡avi, 203 pages : ‡billustrations, figures, tables ; ‡c28 cm.
336 ‡atext ‡btxt ‡2rdacontent
337 ‡aunmediated ‡bn ‡2rdamedia
338 ‡avolume ‡bnc ‡2rdacarrier
490 0 ‡aTechnical documentary report (Air Force Flight Dynamics Laboratory (U.S.)) ; ‡vAFFDL-RTD-TDR-63-4179, Part II
500 ‡a"February 1964."
504 ‡aIncludes bibliograpical references (page 5).
536 ‡aAir Force Contract No. ‡bAF 33(616)-8130, Project No. 8219, Task No. 821902.
538 ‡aMode of access: Internet.
650 0 ‡aHeat ‡xTransmission.
650 0 ‡aAirplanes ‡xWings, Swept-back.
710 2 ‡aUnited States. ‡bAir Force. ‡bSystems Command, ‡eissuing body.
710 2 ‡aAir Force Flight Dynamics Laboratory (U.S.), ‡esponsor.
710 2 ‡aGrumman Aircraft Engineering Corporation, ‡esponsor.
730 0 ‡aTechnical Report Archive & Image Library (TRAIL)
899 ‡a39015104956746
CID ‡a102892564
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