Wind tunnel investigation of aerodynamic loads on weapons separated from carriage under the wing of a tactical fighter aircraft at supersonic speeds

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035 ⊔ ⊔ ‡a(MiU)99187625416706381
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035 ⊔ ⊔ ‡a(OCoLC)1333449688
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040 ⊔ ⊔ ‡aTRAAL ‡beng ‡erda ‡cTRAAL
049 ⊔ ⊔ ‡aMAIN
086 0 ⊔ ‡aD 301.45/33: 73-098
100 1 ⊔ ‡aDonaldson, J. C., ‡eauthor.
245 1 0 ‡aWind tunnel investigation of aerodynamic loads on weapons separated from carriage under the wing of a tactical fighter aircraft at supersonic speeds / ‡cJ.C. Donaldson.
264 ⊔ 1 ‡aArnold Air Force Base, Tennessee : ‡bArnold Engineering Development Center, Air Force Systems Command, United States Air Force, ‡c1973.
300 ⊔ ⊔ ‡aviii, 41 pages : ‡billustrations, ‡c28 cm
336 ⊔ ⊔ ‡atext ‡btxt ‡2rdacontent
337 ⊔ ⊔ ‡aunmediated ‡bn ‡2rdamedia
338 ⊔ ⊔ ‡avolume ‡bnc ‡2rdacarrier
490 0 ⊔ ‡aAEDC-TR ; ‡v73-098
500 ⊔ ⊔ ‡aReport was prepared by ARO, Inc., a subsidiary of Sverdrup & Parcel and Associates, Inc.
500 ⊔ ⊔ ‡a"Final Report for Period January 23 to February 20, 1973."
500 ⊔ ⊔ ‡a"June 1973."
504 ⊔ ⊔ ‡aIncludes bibliograqphic references (page 10).
520 ⊔ ⊔ ‡aExploratory static-stability tests were made on models of the MK-84 weapon and a modular weapon configuration during simulated weapon separation from the wing of the F-4C Tactical Fighter Aircraft at freestream Mach numbers 1.76, 2.0, and 2.5. Data were obtained with the parent aircraft at zero angle of attack and the weapon at the carriage incidence angle of -1 deg. Supplementary data were obtained for weapon angles of attack of + or - deg. Unit Reynolds number ranged from 4.6 million per ft at M free stream mach number = 1.76 to 6.2 million per ft at M free stream mach number = 2.5. Selected results are presented which show the effects on the weapon aerodynamic loads of free-stream Mach number, weapon angle of attack, weapon axial position, and the presence of other stores. Representative shadowgraph and schlieren photographs of the interference flow field are also presented. (Author).
533 ⊔ ⊔ ‡aPhotocopy.
538 ⊔ ⊔ ‡aMode of access: Internet.
650 ⊔ 0 ‡aAerodynamic load.
650 ⊔ 0 ‡aJet fighter planes ‡xWind tunnel testing.
710 2 ⊔ ‡aARO, Inc., ‡esponsor.
710 2 ⊔ ‡aArnold Engineering Development Center, ‡esponsor.
710 1 ⊔ ‡aUnited States. ‡bAir Force. ‡bSystems Command, ‡eissuing body.
730 0 ⊔ ‡aTechnical Report Archive & Image Library (TRAIL)
899 ⊔ ⊔ ‡a39015104952760
CID ⊔ ⊔ ‡a102892568
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DAT 1 ⊔ ‡a20241208060856.0 ‡b2024-12-08T14:15:46Z
DAT 2 ⊔ ‡a2024-07-31T17:30:01Z
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