Unsteady aerodynamics for advanced configurations. Part V. Unsteady potential flow around slender bodies at angles of attack

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049 ‡aMAIN
086 0 ‡aD 301.45/34-2: 64-152, Part V
100 1 ‡aLi, T. C., ‡eauthor.
245 1 0 ‡aUnsteady aerodynamics for advanced configurations. ‡nPart V. ‡pUnsteady potential flow around slender bodies at angles of attack / ‡cT.C. Li.
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, ‡c1965.
300 ‡aviii, 42 pages : ‡billustrations, figures ; ‡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-64-152, Part V
504 ‡aIncludes bibliograpical references (page 42).
536 ‡aAir Force Contract No. ‡bAF 33(657)-10399, Project No. 1370, Task No. 137003.
538 ‡aMode of access: Internet.
650 0 ‡aNonlinear systems.
650 0 ‡aAerodynamics ‡xMathematical models.
650 0 ‡aFlutter (Aerodynamics)
650 0 ‡aUnsteady flow (Aerodynamics)
710 2 ‡aUnited States. ‡bAir Force. ‡bSystems Command, ‡eissuing body.
710 2 ‡aAir Force Flight Dynamics Laboratory (U.S.), ‡esponsor.
710 2 ‡aNorth American Aviation. ‡bSpace and Information Systems Division, ‡esponsor.
730 0 ‡aTechnical Report Archive & Image Library (TRAIL)
899 ‡a39015104956464
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