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Results for “WINGS - DESIGN WING, TAPERED”

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 109 records · Page 6

All sources NASA NTRS DOE OSTI

NASA NTRS1950

An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular-arc Sections and 40 Degree Sweepback : Static Longitudinal Stability and Control Characteristics at a Mach Number of 1.59

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Spearman, M Leroy↗

NASA NTRS1950

Flight Investigation of the Effect of Thickening the Aileron Trailing Edge on Control Effectiveness for Sweptback Tapered Wings Having Sharp-and Round-nose Sections

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Strass, H Kurt↗

NASA NTRS1950

An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular-arc Sections and 40 Degree Sweepback : Static Lateral Stability Characteristics at Mach Numbers of 1.40 and 1.59

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Spearman, M Leroy↗

NASA NTRS1950

Rolling Effectiveness of a Thin Tapered Wing Having Partial-span Ailerons as Determined by Rocket-powered Test Vehicles

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Sandahl, Carl A↗

NASA NTRS1950

Transonic flight test to compare the zero-lift drag of underslung and symmetrical nacelles varied chordwise at 40 percent semispan of a 45 degree sweptback, tapered wing

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Pepper, William B , Jr↗

NASA NTRS1950

An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular-arc Sections and 40 Degree Sweepback : a Pressure-distribution Study of the Aerodynamic Characteristics of the Wing at Mach Number 1.59

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Cooper, Morton↗

NASA NTRS1950

A technique utilizing rocket-propelled test vehicles for the measurement of the damping in roll of sting-mounted models and some initial results of delta and unswept tapered wings

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Bland, William M , Jr↗

NASA NTRS1950

Preliminary results of the flight investigation between Mach numbers of 0.80 and 1.36 of a rocket-powered model of a supersonic airplane configuration having a tapered wing with circular-arc sections and 40 degree sweepback

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D'Aiutolo, Charles T↗

NASA NTRS1950

Wind-tunnel Investigation at Mach Numbers from 0.50 to 1.29 of an Unswept Tapered Wing of Aspect Ratio 2.67 with Leading- and Trailing-edge Flaps - Trailing-edge Flaps Deflected

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Stivers, Louis S , Jr↗

NASA NTRS1950

An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular-arc Sections and 40 Degree Sweepback : Static Lateral Control Characteristics at Mach Numbers of 1.40 and 1.59

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Robinson, Ross B↗

NASA NTRS1951

Wind-tunnel Investigation at Mach Numbers from 0.50 to 1.29 of an Unswept, Tapered Wing of Aspect Ratio 2.67 with Leading- and Trailing-edge Flaps : Flaps Deflected in Combination

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Stivers, Louis S , Jr↗

NASA NTRS1951

Wind-tunnel Investigation at Mach Numbers from 0.50 to 1.29 of an Unswept, Tapered Wing of Aspect Ratio 2.67 with Leading- and Trailing-edge Flaps - Leading-edge Flaps Deflected

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Stivers, Louis S , Jr↗

NASA NTRS1951

Experimental downwash and wake characteristics at subsonic and supersonic Mach numbers behind an unswept, tapered wing, of aspect ratio 2.67 with leading-and trailing-edge flaps

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Stivers, Louis S , Jr↗

NASA NTRS1951

An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular-arc Sections and 40 Degree Sweepback : Force Characteristics of the Complete Configuration and Its Various Components at Mach Numbers of 1.40 and 1.59

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Smith, Norman F↗

NASA NTRS1951

Aerodynamic Characteristics of Tapered Wings Having Aspect Ratios of 4, 6, and 8, Quarter-chord Lines Swept Back 45 Degrees, and NACA 63(sub 1)A012 Airfoil Sections : Transonic-bump Method

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Polhamus, Edward C↗

NASA NTRS1951

An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular-arc Section and 40 Degree Sweepback : a Pressure-distribution Study of the Aerodynamic Characteristics of the Wing at Mach Number 1.40

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Smith, Norman F↗

NASA NTRS1951

Damping in Roll of Rocket-powered Test Vehicles Having Swept, Tapered Wings of Low Aspect Ratio

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Sanders, E Claude↗

NASA NTRS1952

Effects of three types of blunt trailing edges on the aerodynamic characteristics of a plane tapered wing of aspect ratio 3.1, with a 3-percent- thick biconvex section

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Dugan, Duane W↗