Comparison of two methods used to measure aerodynamic loads acting on captive store models in wind tunnel tests

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086 0 ⊔ ‡aD 301.45/33: 76-122
100 1 ⊔ ‡aDix, R. E., ‡eauthor.
245 1 0 ‡aComparison of two methods used to measure aerodynamic loads acting on captive store models in wind tunnel tests / ‡cR.E. Dix.
264 ⊔ 1 ‡aArnold Air Force Base, Tennessee : ‡bArnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, ‡c1976.
300 ⊔ ⊔ ‡a261 pages : ‡billustrations ; ‡c28 cm
336 ⊔ ⊔ ‡atext ‡btxt ‡2rdacontent
337 ⊔ ⊔ ‡aunmediated ‡bn ‡2rdamedia
338 ⊔ ⊔ ‡avolume ‡bnc ‡2rdacarrier
490 0 ⊔ ‡aAEDC-TR ; ‡v76-133
500 ⊔ ⊔ ‡a"September 1976."
500 ⊔ ⊔ ‡a"Final Report: April 1973 -- May 1976."
504 ⊔ ⊔ ‡aIncludes bibliographical references (page 28).
520 ⊔ ⊔ ‡aIn a series of wind tunnel tests, measurements were made of the aerodynamic loads acting on eight different store configurations supported in and near the external captive position on a 1/20-scale model of the F-4C aircraft. Store models included blunt and contoured afterbody shapes, stable and unstable configurations, and large (pylon-mounted) and small (rack-mounted) configurations. Six components of forces and moments were measured using two methods of supporting the store models: an internal bracket support technique (IBS), and a dual sting support technique. Some characteristics of the interference flow field of the aircraft were also inferred.
536 ⊔ ⊔ ‡aReport supported by the Air Force Systems Command and prepared by ARO, Inc, under Program Element, ‡e65807F.
538 ⊔ ⊔ ‡aMode of access: Internet.
650 ⊔ 0 ‡aPhantom II (Jet fighter plane)
650 ⊔ 0 ‡aAerodynamic load.
710 1 ⊔ ‡aUnited States. ‡bAir Force. ‡bSystems Command, ‡eissuing body.
710 2 ⊔ ‡aArnold Engineering Development Center, ‡esponsor.
710 2 ⊔ ‡aARO, Inc., ‡esponsor.
730 0 ⊔ ‡aTechnical Report Archive & Image Library (TRAIL)
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