The Longitudinal Characteristics at Mach Numbers up to 0.92 of Several Wing-fuselage-tail Combinations Having Sweptback Wings with NACA Four-digit Thickness Distributions
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Sutton, Fred B↗
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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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Some considerations regarding the application of the supersonic area rule to the design of airplane fuselages
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Whitcomb, Richard T↗
The Use of Area Suction for Improving the Longitudinal Characteristics of a Thin Unswept Wing-fuselage Model with Leading- and Trailing-edge Flaps
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Koenig, David G↗
Effectiveness at Transonic Speeds of Flap-type Ailerons for Several Spanwise Locations on a 4-percent-thick Sweptback-wing--fuselage Model with and Without Tails
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Hieser, Gerald↗
Pressure Distributions on Four Canopy-fuselage Configurations at Transonic Speeds
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Cornette, Elden S↗
Investigation at Supersonic Speeds of the Effects of Bomb-bay Configuration upon the Aerodynamic Characteristics of Fuselages with Noncircular Cross Sections
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Rainey, Robert W↗
Low-speed Pressure-distribution Investigation of a Thin-delta-wing--fuselage Model with Double Slotted Flap, Extended Double Slotted Flap, and Canard
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Croom, Delwin R↗
Experimental Static Aerodynamic Forces and Moments at High Subsonic Speeds on a Missile Model During Simulated Launching from Unswept-, Sweptback-, and Modified-delta-wing--fuselage Combinations at Zero Sideslip
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Alford, William J↗
Experimental Investigation of Flow Fields at Zero Sideslip near Swept- and Unswept-wing--fuselage Combinations at Low Speed
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Alford, William J↗
Investigation of static pressures and boundary-layer characteristics of the forward parts of nine fuselages of various cross-sectional shapes at M (sub infinity) equals 2.01
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Hasel, Lowell E↗
Investigation at high subsonic speeds of the effects of various horizontal fuselage forebody fins on the directional and longitudinal stability of a complete model having a 45 degree sweptback wing
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Sleeman, William C , Jr↗
A Flight Investigation to Determine the Effectiveness of Mach Number 1.0, 1.2, and 1.41 Fuselage Indentations for Reducing the Pressure Drag of a 45 Degree Sweptback Wing Configuration at Transonic and Low Supersonic Speeds
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Blanchard, Willard S , Jr↗
A Wind-tunnel Investigation of the Low-amplitude Damping in Yaw and Directional Stability of a Fuselage-tail Configuration at Mach Numbers up to 1.10
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Palmer, William E↗
Zero-lift Drag of a Large Fuselage Cavity and a Partially Submerged Store on a 52.5 Degree Sweptback-wing - Body Configuration as Determined from Free-flight Tests at Mach Numbers of 0.7 to 1.53
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Hoffman, Sherwood↗
Low-speed Pressure-distribution Investigation of a Thin-delta-wing--fuselage Model Having Double Slotted Flaps and Spoilers
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Croom, Delwin R↗
Exploratory Investigation of the Effect of Wing Slots and Leading-edge Slats on the Longitudinal Stability Characteristics of a 45 Degree Sweptback Wing-fuselage Configuration
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Critzos, Chris C↗
Flight Investigation and Theoretical Calculations of the Fuselage Deformations of a Swept-wing Bomber During Push-pull Maneuvers
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Mayo, Alton, P↗
Free-flight Investigation of the Drag of a Model of a 60 Degree Delta-wing Bomber with Strut-mounted Siamese Nacelles and Indented Fuselage at Mach Numbers from 0.80 to 1.35
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Hoffman, Sherwood↗