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Results for “WINGS - POLARS”

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 343 records · Page 19

All sources NASA NTRS DOE OSTI

NASA NTRS1955

Wing pressure distributions over the lift range of the convair xf-92a delta-wing airplane at subsonic and transonic speeds

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Jordan, G. H.↗

NASA NTRS1959

A wind tunnel investigation to evaluate the aerodynamic performance of three different airplane configurations having arrow-wing and delta-wing plan forms at a Mach number of 2.91

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Grimaud, J. E.↗

NASA NTRS1958

Idealized Wings and Wing-Bodies at a Mach Number of 3

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Elliot D Katzen↗

NASA NTRS1972

Space shuttle: Static stability and control investigation of NR/GD delta wing booster (B-20) and delta wing orbiter (134D), volume 4

Test results of booster and orbiter models of various component buildup configurations are reported. Dataset Collation Sheets, which give a complete summary of the configurations, are presented along with a description of the test facility. Data reduction procedures are described.

Allen, E. C., Jr.↗

NASA NTRS1973

Space shuttle: Pressure investigation of a space shuttle launch configuration consisting of a delta-wing orbiter and a swept-wing booster with canard and tip fins (M equals 0.6 to 1.3). Volume 1, part B: Booster data

For abstract, see .

Rampy, J. M.↗

NASA NTRS1973

Space shuttle: Pressure investigation of a space shuttle launch configuration consisting of a delta-wing orbiter and a swept-wing booster with canard and tip fins (M equals 0.6 to 1.3). Volume 2: Orbiter data

For abstract, see

Rampy, J. M.↗

NASA NTRS1956

Large-scale wind-tunnel tests of an airplane model with a 45 deg 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, D. G.↗

NASA NTRS1955

Aerodynamics of bodies, wings, and wing-body combinations at high angles of attack and supersonic speeds

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Nielsen, J. N.↗

NASA NTRS1966

Aerodynamic-center considerations of wings and wing-body combinations

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Lamar, J. E.↗

NASA NTRS1966

An integrated approach to the analysis and design of wings and wing-body combinations in supersonic flow

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Carmichael, R. L.↗

NASA NTRS1975

Some methods for reducing wing drag and wing-Nacelle interference

Primary efforts directed toward drag reduction centered on the design of both supercritical and subcritical families of airfoils, the reduction of induced drag through the use of vortex diffusers, and the reduction of interference drag for executive-type aircraft.

Kelly, T. C.↗

NASA NTRS1979

Effects of wing leading-edge deflection on low-speed aerodynamic characteristics of a low-aspect-ratio highly swept arrow-wing configuration

Static force tests were conducted in the Langley V/STOL tunnel at a Reynolds number (based on the mean aerodynamic chord) of about 2.0 x 10 to the 6th power for an angle-of-attack range from about - 10 deg to 17 deg and angles of sideslip of 0 and + or - 5 deg. Limited flow visualization studies were also conducted in order to provide a qualitative assessment of leading-edge upwash characteristics.

Coe, P. L., Jr.↗

NASA NTRS1984