Steady loads due to jet interference on wings, tails, and fuselages at transonic speeds
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Swihart, John M↗
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Results for “FUSELAGE”
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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A buffet investigation at high subsonic speeds of wing-fuselage-tail combinations having sweptback wings with NACA 64A thickness distributions, fences, a leading-edge extension, and body contouring
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Sutton, Fred B↗
The Effects at Subsonic Speeds of Wing Fences and a Tail on the Longitudinal Characteristics of a 63 Degree Swept-wing Fuselage Combination
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Buell, Donald A↗
An Investigation of Supersonic Store Interference in the Vicinity of a 22 Degree Swept-wing--fuselage Configuration at Mach Numbers of 1.61 and 2.01
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Geier, Douglas J↗
Preliminary Flight Survey of Fuselage and Boundary-layer Sound-pressure Levels
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Mcleod, Norman J↗
Effect at high subsonic speeds of fuselage forebody strakes on the static stability and vertical-tail-load characteristics of a complete model having a delta wing
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Polhamus, Edward C↗
Wind-tunnel Investigation of the Use of Leading-edge and Trailing-edge Area-suction Flaps on a 13-percent-thick Straight Wing and Fuselage Model
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Holzhauser, Curt A↗
Aerodynamic and inlet-flow-field characteristics at a free-stream Mach number of 3.0 for airplanes with circular fuselage cross sections and for two engine locations
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Dryer, Murray↗
Effects of External Store-pylon Configuration and Position on the Aerodynamic Characteristics of a 45 Degree Swept Wing-fuselage Combination at a Mach Number of 1.61
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Morris, Odell A↗
Transonic Lateral and Longitudinal Aerodynamic Characteristics of a Lateral-control System Employing Rotatable Airfoils Mounted Vertically at the Wing Tips of an Unswept Wing-fuselage-tail Combination
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Axelson, John A↗
Investigation of spoiler-slot-deflector ailerons and other spoiler ailerons on a 45 degree sweptback-wing--fuselage combination at Mach numbers from 0.60 to 1.03
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West, F E↗
The origin and distribution of supersonic store interference from measurement of individual forces on several wing-fuselage-store configurations II : swept-wing-heavy-bomber configuration with large store (nacelle). lateral forces and pitching moment
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Smith, Norman F↗
Rocket-model Investigation to Determine the Lift and Pitching Effectiveness of Small Pulse Rockets Exhausted from the Fuselage over the Surface of an Adjacent Wing at Mach Numbers from 0.9 to 1.8
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Martz, C William↗
Internal performance at Mach number to 2.0 of two auxiliary inlets immersed in fuselage boundary layer
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Pennington, Donald B↗
Effects of a Leading-edge Slat and a Trailing-edge Split Flap on the Aerodynamic Characteristics of a Wing-fuselage Combination Having a Nearly Triangular Wing of Aspect Ratio 2.9 at Mach Numbers from 0.60 to 0.92
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Demele, Fred A↗
Aerodynamic Characteristics of Two All-movable Wings Tested in the Presence of a Fuselage at a Mach Number of 1.9
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Conner, D William↗
Wind-tunnel investigation at high subsonic speeds of the effects of wing-mounted external stores on the loading and aerodynamic characteristics in pitch of a 45 degree sweptback wing combined with a fuselage
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Silvers, H Norman↗
Investigations on the downwash behind a tapered wing with fuselage and propeller
The new downwash measurements behind a tapered wing with parallel center section described in the present report can be brought into good agreement with theoretical calculations if made on the basis of not-rolled-up vortex sheet and allowance is made for the lowering of the sheet. The test values are about 1 degree higher than the "upper limit" established for it, as against approximately 0.5 degrees in the earlier tests behind a rectangular and elliptical wing. The measurements on lateral axes, especially if lying below the wing on a level with the vortex train, disclosed in accord with the lift distribution, a marked change in angle over the span of the tail in contrast to the rectangular and elliptical wing.
Muttray, H↗