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Results for “WINGS - SWEEPBACK”

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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At least 559 records · Page 31

All sources NASA NTRS DOE OSTI

NASA NTRS1957

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↗

NASA NTRS1957

Analysis of Wing Loads Measured on a Flexible Swept-wing Jet Bomber During Push-pull Maneuvers

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Gainer, Patrick A↗

NASA NTRS1957

Effect of Full-span Trailing-edge Elevons on the Transonic Longitudinal Aerodynamic Characteristics of a Wing-body Combination Having a 3-percent-thick Triangular Wing with 60 Degree Leading-edge Sweep

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Critzos, Chris C↗

NASA NTRS1957

Flight Investigation of the Low-speed Characteristics of a 35 Degree Swept-wing Airplane Equipped with an Area-suction Ejector Flap and Various Wing Leading-edge Devices

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Anderson, Seth B↗

NASA NTRS1957

Comparison of Low-lift Drag at Mach Numbers from 0.74 to 1.37 of Rocket-boosted Models Having Externally Braced Wings and Cantilever Wings

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Dickens, Waldo L↗

NASA NTRS1957

Effects of Wing Warp on the Lift, Drag, and Static Longitudinal Stability Characteristics of an Aircraft Configuration Having an Arrow Wing of Aspect Ratio 1.86 at Mach Numbers from 1.1 to 1.7

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Gillespie, Warren, Jr↗

NASA NTRS1957

Aerodynamic heat transfer to wing surfaces and wing leading edges

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Bond, Aleck C↗

NASA NTRS1958

Investigation of the Longitudinal Aerodynamic Characteristics of a Trapezoidal-wing Airplane Model with Various Vertical Positions of Wing and Horizontal Tail at Mach Numbers of 1.41 and 2.01

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Foster, Gerald V↗

NASA NTRS1957

High-pressure Blowing over Flap and Wing Leading Edge of a Thin Large-scale 49 Degree Swept Wing-body-tail Configuration in Combination with a Drooped Nose and a Nose with a Radius Increase

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Fink, Marvin P↗

NASA NTRS1958

Longitudinal and Lateral Stability and Control Characteristics at Mach Number 2.01 of a 60 Degree Delta-wing Airplane Configuration Equipped with a Canard Control and with Wing Trailing-edge Flap Controls

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Spearman, M Leroy↗

NASA NTRS1957

Preliminary investigation of the characteristics of a two dimensional wing and propeller with the propeller plane of rotation in the wing-chord plane

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Hickey, David H↗

NASA NTRS1957

Effects of wing-tip droop on the longitudinal characteristics of two highly swept wing-body combinations at Mach numbers from 0.6 to 1.4

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Knechtel, Earl D↗

NASA NTRS1957

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↗

NASA NTRS1957

Effects of wing inboard plan-form modifications on lift, drag, and longitudinal stability at Mach numbers from 1.0 to 2.3 of a rocket-propelled free-flight model with a 52.5 degree sweptback wing of aspect ratio 3

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Henning, Allen B↗

NASA NTRS1957

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↗

NASA NTRS1957

Investigation of the aerodynamic characteristics in pitch and sideslip of a 45 degree swept-wing airplane configuration with various vertical locations of the wing and horizontal tail : static lateral and directional stability; Mach numbers of 1.41 a

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Spearman, M Leroy↗

NASA NTRS1958

Surface pressure distributions on a large-scale 49 degree sweptback wing-body-tail configuration with blowing applied over the flaps and wing leading edge

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Mclemore, H Clyde↗

NASA NTRS1958

Effects of Vertical Location of the Wing and Horizontal Tail on the Static Lateral and Directional Stability of a Trapezoidal-wing Airplane Model at Mach Numbers of 1.41 and 2.01

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Robinson, Ross B↗