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Results for “flaps”

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 1,189 records · Page 66

All sources NASA NTRS DOE OSTI

NASA NTRS1950

Effects of plain and step spoiler location and projection on the lateral control characteristics of a plain and flapped 42 degree sweptback wing at a Reynolds number of 6.8 x 10(exp 6)

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Bollech, Thomas V↗

NASA NTRS1950

Investigation of flap-type ailerons on an untapered wing having an aspect ratio of 3.7, 45 degree sweepback, and an NACA 65A009 airfoil section : transonic-bump method

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Macleod, Richard G↗

NASA NTRS1950

A method for predicting the low speed chordwise pressure distribution over sharp edge airfoil sections with plain flaps at the leading and trailing edges

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Nuber, Robert J↗

NASA NTRS1951

Effects of a fuselage flap dive brake on the aerodynamic characteristics of 1/30 scale semispan model of the Bell X-5 variable-sweep airplane at a Mach number 1.24 as determined by the NACA wing flow method

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Kennedy, Robert M↗

NASA NTRS1951

Influence of Airfoil Trailing-edge Angle and Trailing-edge-thickness Variation on the Effectiveness of a Plain Flap at High Subsonic Mach Numbers

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Hemenover, Albert D↗

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

Low-speed Investigation of Several Types of Split Flap on a 47.7 Degree Sweptback-wing - Fuselage Combination of Aspect Ratio 5.1 at a Reynolds Number of 6.0 x 10(exp 6)

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Spooner, Stanley H↗

NASA NTRS1951

Investigation at Supersonic Speeds of Some of the Factors Affecting the Flow over a Rectangular Wing with Symmetrical Circular-arc Section and 30-percent-chord Trailing-edge Flap

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Czarnecki, K R↗

NASA NTRS1950

Low-speed Investigation of the Effect of Several Flap and Spoiler Ailerons on the Lateral Characteristics of a 47.5 Degree Sweptback-wing-fuselage Combination at a Reynolds Number of 4.4. x 10(6)

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Pasamanick, Jerome↗

NASA NTRS1951

Low-speed Investigation of the Effects of Single Slotted and Double Slotted Flaps on a 47.7 Degree Sweptback-wing : Fuselage Combination at a Reynolds Number of 6.0 x 10(exp 6)

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Mollenberg, Ernst F↗

NASA NTRS1951

Buffeting-load measurements on a jet-powered bomber airplane with reflexed flaps

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See, John A↗

NASA NTRS1952

A Preliminary Low-speed Wind-tunnel Investigation of a Thin Delta Wing Equipped with a Double and a Single Slotted Flap

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Macleod, Richard G↗

NASA NTRS1951

Effects of Double-slotted Flaps and Leading-edge Modifications on the Low-speed Characteristics of a Large-scale 45 Degrees Swept-back Wing with and Without Camber and Twist

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James, Harry A↗

NASA NTRS1951

Some effects of spanwise aileron location and wing structural rigidity on the rolling effectiveness of 0.3-chord flap-type ailerons on a tapered wing having 63 degrees sweepback at the leading edge and NACA 64A005 airfoil sections

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Strass, H Kurt↗

NASA NTRS1951

Aerodynamic characteristics at transonic speeds of a tapered 45 degree sweptback wing of aspect ratio 3 having a full-span flap-type control

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Lockwood, Vernard E↗

NASA NTRS1952

Aerodynamic characteristics at transonic speeds of a 60 degree delta wing equipped with a constant-chord flap-type control with and without an unshielded horn balance : transonic-bump method

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Wiley, Harleth G↗

NASA NTRS1951

Low-speed longitudinal and wake air-flow characteristics at a Reynolds number of 6.0 x 10(exp 6) of a 52 degree sweptback wing equipped with various spans of leading-edge flaps, a fuselage, and a horizontal tail at various vertical positions

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Griner, Roland F↗

NASA NTRS1952

Studies of the Flow Field Behind a Large Scale 47.5 Degree Sweptback Wing Having Circular-arc Airfoil Sections and Equipped with Drooped-nose and Plain Flaps

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Lange, Roy H↗