Comparisons of free-flight and wind tunnel data on slender cones

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050 ⊔ 4 ‡aTL570 ‡b.G74 1964
086 0 ⊔ ‡aD 301.45/33-2:64-272
100 1 ⊔ ‡aGriffith, B. J., ‡eauthor.
245 1 0 ‡aComparisons of free-flight and wind tunnel data on slender cones / ‡cby B.J. Griffith and Leo G. Siler.
264 ⊔ 1 ‡aArnold Air Force Station, Tennessee : ‡bArnold Engineering Development Center, Air Force Systems Command, United States Air Force, ‡c1964.
300 ⊔ ⊔ ‡ax, 22 pages : ‡billustrations ; ‡c28 cm.
336 ⊔ ⊔ ‡atext ‡btxt ‡2rdacontent
337 ⊔ ⊔ ‡aunmediated ‡bn ‡2rdamedia
338 ⊔ ⊔ ‡avolume ‡bnc ‡2rdacarrier
490 0 ⊔ ‡aAEDC-TDR ; ‡v64-272
500 ⊔ ⊔ ‡a"ARO, Inc. a subsidiary of Sverdrup and Parcel, Inc."
500 ⊔ ⊔ ‡a"Von Kármán Gas Dynamics Facility."
500 ⊔ ⊔ ‡a"December 1964."
500 ⊔ ⊔ ‡a"AEDC-TDR-64-272."
500 ⊔ ⊔ ‡aThis work is part of the library's "Parachute History Collection" donated by Sandia National Laboratories through the American Institute of Aeronautics and Astronautics Aerodynamic Deceleration Systems Technical Committee.
504 ⊔ ⊔ ‡aIncludes bibliographical references (pages 7-8).
520 3 ⊔ ‡aHigh Mach number wind tunnel drag, lift, moment, and heat-transfer data from sting-mounted models are compared, with available free-flight data. The resulting comparisons show that there is an apparent lack of support interference effects on forebody flow fields of slender cones, and that the so-called real gas effects on the observed data are insignificant at velocities up to 18,000 ft/sec.
536 ⊔ ⊔ ‡aARO, Inc. ‡bAF 40(600)-100 ‡e65402034 ‡fVT3503
538 ⊔ ⊔ ‡aMode of access: Internet.
650 ⊔ 7 ‡aWind tunnels. ‡2fast ‡0(OCoLC)fst01175710
650 ⊔ 7 ‡aAerodynamics ‡xTesting. ‡2fast ‡0(OCoLC)fst00798213
650 ⊔ 6 ‡aSouffleries aérodynamiques. ‡0(CaQQLa)201-0050931
650 ⊔ 0 ‡aWind tunnels.
650 ⊔ 0 ‡aAerodynamics ‡xTesting.
700 1 ⊔ ‡aSiler, Leo G., ‡eauthor.
710 2 ⊔ ‡aARO, Inc., ‡esponsor.
710 2 ⊔ ‡aArnold Engineering Development Center, ‡esponsor.
710 1 ⊔ ‡aUnited States. ‡bAir Force. ‡bSystems Command, ‡eissuing body.
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