Static aerodynamic characteristics of a series of generalized slender bodies with and without fins at Mach numbers form 0.6 to 3.0 and angles of attack from 0 to 180 deg. Volume 1

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040 ‡aTRAAL ‡beng ‡erda ‡cTRAAL
049 ‡aMAIN
086 0 ‡aD 301.45/33: 75-124 Revised
100 1 ‡aBaker, William B., ‡cJr., ‡eauthor.
245 1 0 ‡aStatic aerodynamic characteristics of a series of generalized slender bodies with and without fins at Mach numbers form 0.6 to 3.0 and angles of attack from 0 to 180 deg. ‡nVolume 1 / ‡cWilliam B. Baker, Jr.
264 1 ‡aArnold Air Force Base, Tennessee : ‡bArnold Engineering Development Center, Air Force Systems Command, United States Air Force, ‡c1976.
300 ‡a44 pages : ‡billustrations ; ‡c28 cm
336 ‡atext ‡btxt ‡2rdacontent
337 ‡aunmediated ‡bn ‡2rdamedia
338 ‡avolume ‡bnc ‡2rdacarrier
490 0 ‡aAEDC-TR ; ‡v75-124 Revised
500 ‡aReport was prepared by ARO, Inc., a subsidiary of Sverdrup & Parcel and Associates, Inc.
500 ‡aFinal Report: 1 January 1972 to 31 January 1975."
500 ‡a"May 1976."
504 ‡aIncludes bibliographic references (page 23).
538 ‡aMode of access: Internet.
650 0 ‡aRockets (Aeronautics) ‡xFins.
650 0 ‡aGuided missiles ‡xAerodynamics.
650 0 ‡aAerodynamics, Supersonic.
710 2 ‡aArnold Engineering Development Center, ‡esponsor.
710 1 ‡aUnited States. ‡bAir Force. ‡bSystems Command, ‡eissuing body.
710 2 ‡aARO, Inc., ‡esponsor.
730 0 ‡aTechnical Report Archive & Image Library (TRAIL)
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