Downwash Survey Behind Two Low-aspect-ratio Variable-incidence Wings in Combination with Three Different Size Fuselages at a Mach Number of 0.25
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Hopkins, Edward J↗
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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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Experimental Static Aerodynamic Forces and Moments at Low Speed on a Canard Missle During Simulated Launching from the Midsemispan and Wing-tip Locations of a 45 Degree Sweptback Wing-fuselage Combination
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Alford, William J , Jr↗
The origin and distribution of supersonic store interference from measurement of individual forces on several wing-fuselage-store configurations I : swept-wing heavy-bomber configuration with large store (nacelle). lift and drag; Mach number, 1.61
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Smith, Norman F↗
Experimental Static Aerodynamic Forces and Moments at Low Speed on a Missile Model During Simulated Launching from the 25-percent-semispan and Wing-tip Locations of a 45 Degree Sweptback Wing-fuselage Combination
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Alford, William J , Jr↗
Drag Investigation of a Swept-wing Fighter-airplane Model Incorporating Two Drag-rise-reducing Fuselage Revisions
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Whitcomb, Charles F↗
Experimental investigation at high subsonic speeds of the effects of leading-edge radius on the aerodynamic characteristics of a sweptback-wing - fuselage combination with leading-edge flaps and chord-extensions
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Spreemann, Kenneth P↗
Effects of wing-fuselage flow fields on missile loads at subsonic speeds
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Alford, William J , Jr↗
Force and pressure measurements on several canopy-fuselage configurations at transonic Mach numbers 1.41 and 2.01
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Robins, A Warner↗
An Experimental Study of a Method for Designing Fuselage Side Air Inlets for High Performance at Transonic and Low Supersonic Speeds
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Howell, Robert R↗
The origin and distribution of supersonic store interference from measurement of individual forces on several wing-fuselage-store configurations IV : delta-wing heavy-bomber configuration with large store. Mach number, 1.61
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Morris, Odell A↗
The Origin and Distribution of Supersonic Store Interference from Measurement of Individual Forces on Several Wing-fuselage-store Configurations III : Swept-wing Fighter-bomber Configuration with Large and Small Stores. Mach Number, 1.61
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Smith, Norman F↗
The Effect of Leading-edge Extensions on the Longitudinal Characteristics at Mach Numbers up to 0.92 of a Wing-fuselage-tail Combination Having a 40 Degree Sweptback Wing with NACA 64A Thickness Distribution
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Sutton, Fred B↗
Low-speed Pressure-distribution Investigation of a Spoiler and a Spoiler-slot-deflector on a 30 Degree Sweptback Wing-fuselage Model Having an Aspect Ratio of 3, a Taper Ratio of 0.5, and NACA 65A004 Airfoil Section
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Hammond, Alexander D↗
Fuselage Side Inlets : a Study of Some Factors Affecting Their Performance and a Comparison with Nose Inlets
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Mossman, Emmet A↗
The Origin and Distribution of Supersonic Store Interference from Measurement of Individual Forces on Several Wing-fuselage-store Configurations V : Swept-wing Heavy-bomber Configuration with Large Store (nacelle). Mach Number 2.01
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Carson, Harry W↗
The Effect of Wing Height on the Longitudinal Characteristics at High Subsonic Speeds of a Wing-fuselage-tail Combination Having a Wing with 40 Degrees of Sweepback and NACA Four-digit Thickness Distribution
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Dickson, Jerald K↗
The Effect of Wing Fences on the Longitudinal Characteristics at Mach Numbers up to 0.92 of a Wing-fuselage-tail Combination Having a 40 Degree Sweptback Wing with NACA 64A Thickness Distribution
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Dickson, Gerald K↗
Experimental study of a method of designing the sweptback-wing-fuselage juncture to reduce the drag at moderate supersonic speeds
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Howell, Robert R↗