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Effect of large store /nacelle/ on a swept-wing heavy bomber - lateral force and pitching moments
Origin and distribution of supersonic store interference/measurement of individual forces on delta-wing heavy bomber configuration mach 1.61
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Origin & distribution of supersonic store interference/measurement of individual forces - swept-wing heavy bomber with large store figure
Supersonic store interference - 1, swept-wing heavy bomber with large stores - lift & drag at mach 1.61
Origin of supersonic store interference from measurements of individual forces - swept-wing fighter-bomber with large & small stores
Store pitch flexibility effect on flutter characteristics of wing-store configurations in transonic wind tunnel
Forces and moments of store-pylon combination mounting on swept wing-fuselage configuration in supersonic pressure tunnel
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A supersonic wind-tunnel investigation on store interference has been conducted in the Langley 4- by 4-foot supersonic pressure tunnel at a Mach number of 1.61. Forces and moments were measured on a large ogive-cylinder store in the presence of a 45 deg swept-wing-fuselage bomber configuration for a number of store locations below the fuselage center line. Results of the investigation show that large variations of store lift, drag, and pitch occur with changes in store or airplane angle of attack, store vertical location, and store horizontal location. The variation of the store forces and moments with respect to the chordwise location of the wing plan form indicates that the wing is a large factor in producing the interference loads on the store. Comparison of data for underfuselage and underwing store locations at an angle of attack of 0 deg showed maximum store drag interferences of similar magnitudes, but showed considerably smaller maximum interference on store lift an pitching moments for underfuselage store locations.