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Results for “wind tunnel testing”

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 649 records · Page 36

All sources NASA NTRS DOE OSTI

NASA NTRS1953

The results of wind-tunnel tests at low speeds of a four-engine propeller-driven airplane configuration having a wing with 40 degrees of sweepback and an aspect ratio of 10

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Edwards, George G↗

NASA NTRS1954

Analysis of wind-tunnel tests at low speeds of a four-engine propeller-driven airplane configuration having a wing with 40 degrees of sweepback

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Edwards, George, G↗

NASA NTRS1956

Full-scale Wind-tunnel Tests of the Longitudinal Stability and Control Characteristics of the XV-1 Convertiplane in the Autorotating Flight Range

Force and moments were measured for the XV-1 convertaplane at 75 to 150 knots. Rotor on and off and propeller powered and off configurations were investigated. The characteristics of the V-tab horizontal tail and its downwash field were studied. Lift interference between fixed wing and rotor and possible means of drag reduction were considered.

STABILITY, LONGITUDINAL - STATIC↗

NASA NTRS1956

Static lateral-directional stability characteristics of five contemporary airplane models from wind-tunnel tests at high subsonic and supersonic speeds

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Smith, Willard G↗

NASA NTRS1956

Full-scale Wind-tunnel Tests of a 35 Degree Swept-wing Fighter Airplane with a Spoiler-slot-deflector Lateral Control System

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Scallion, William I↗

NASA NTRS1954

Large-scale low-speed wind-tunnel tests of a model having a 60 degree delta horizontal canard control surface and wing to obtain static-longitudinal-stability and canard surface hinge-moment data

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Burrows, Dale L↗

NASA NTRS1956

Wind-tunnel Tests of Blowing Boundary-layer Control with Jet Pressure Ratios up to 9.5 on the Trailing-edge Flaps of a 35 Degree Sweptback Wing Airplane

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Kelly, Mark W↗

NASA NTRS1956

Large-scale Wind-tunnel Tests of an Airplane Model with a 45 Degree Sweptback Wing of Aspect Ratio 2.8 with Area Suction Applied to Trailing-edge Flaps and with Several Wing Leading-edge Modifications

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Koenig, David G↗

NASA NTRS1957

Wind-tunnel Tests of the Static Longitudinal Characteristics at Low Speed of a Swept-wing Airplane with Slotted Flaps, Area-suction Flaps, and Wing Leading-edge Devices

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Maki, Ralph L↗

NASA NTRS1957

Wind-tunnel Tests of the Static Longitudinal Characteristics at Low Speed of a Swept-wing Airplane with Blowing Flaps and Leading-edge Slats

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James, Harry A↗

NASA NTRS1958

Large-scale Wind-tunnel Tests of an Airplane Model with a 45 Degree Sweptback Wing of Aspect Ratio 2.8 Employing High-velocity Blowing over the Leading- and Trailing-edge Flaps

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Hickey, David H↗

NASA NTRS1956

Full-scale Wind-tunnel Tests of a 35 Degree Sweptback-wing Airplane with High-velocity Blowing over the Trailing-edge Flaps : Longitudinal and Lateral Stability and Control

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Tolhurst, William H , Jr↗

NASA NTRS1958

Large-scale Wind-tunnel Tests of a Jet-transport-type Model with Leading- and Trailing-edge High-lift Devices

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Aoyagi, Kiyoshi↗

NASA NTRS1950

Wind-tunnel Tests of a 0.16-scale Model of the X-3 Airplane at High Subsonic Speeds : Stability and Control Characteristics

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Hamilton, William T↗

NASA NTRS1950

Wind-tunnel Tests of a 0.16-scale Model of the X-3 Airplane at High Subsonic Speeds : Additional Stability and Control Characteristics and the Aerodynamic Effects of External Stores and Ram Jets

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Cleary, Joseph W↗

NASA NTRS1957

Transonic wind-tunnel tests of the launch, jettison, and longitudinal characteristics of an airplane- and missile-model combination

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Dewey, C Forbes, Jr↗

NASA NTRS1951

Wind-tunnel Tests of a 1/12-scale Model of the X-3 Airplane at Subsonic and Supersonic Speeds.

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Olson, Robert N↗

NASA NTRS1929

Full-Scale Wind-Tunnel Tests of a Series of Metal Propellers on a VE-7 Airplane

An adjustable blade metal propeller was tested at five different angle settings, forming a series varying in pitch. The propeller was mounted on a VE-7 airplane in the twenty-foot propeller research tunnel of the National Advisory Committee for Aeronautics. The efficiencies were found to be from 4 to 7 per cent higher than those of standard wood propellers operating under the same conditions. The results are given in convenient form for use in selecting propellers for aircraft.

Weick, Fred E↗