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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 199 records · Page 11

All sources NASA NTRS DOE OSTI

NASA NTRS1953

Longitudinal Stability and Wake-flow Characteristics of a Twisted and Cambered Wing-fuselage Combination of 45 Degree Sweepback and Aspect Ratio 8 with a Horizontal Tail and Stall-control Devices at a Reynolds Number of 4.0 x 10(exp 6).

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Foster, Gerald V↗

NASA NTRS1954

Rocket-model investigation of the longitudinal stability, drag, and duct performance of a 60 degree delta-wing canard aircraft with twin side inlets at Mach numbers from 0.80 to 1.70

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Bond, Aleck C↗

NASA NTRS1946

Effect of sweepback and aspect ratio on longitudinal stability characteristics of wings at low speeds

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Shortal, Joseph A↗

NASA NTRS1953

Some low-speed wind-tunnel experiments pertaining to the longitudinal stability characteristics of a 35-degree swept-wing model and an unswept-wing model

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Jaquet, Byron, M↗

NASA NTRS1954

Low-speed Investigation of the Effects of Location of a Delta and a Straight Tail on the Longitudinal Stability and Control of a Thin Delta Wing with Extended Double Slotted Flaps

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Riebe, John M↗

NASA NTRS1954

Determination of Longitudinal Stability in Supersonic Accelerated Maneuvers for the Douglas D-558-II Research Airplane

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Ankenbruck, Herman O↗

NASA NTRS1953

Longitudinal stability and trim of two rocket propelled airplane models having 45 degree sweptback wings and tails with the horizontal tail mounted in two positions

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Parks, James H↗

NASA NTRS1954

Effect of Wing Slats and Inboard Wing Fences on the Longitudinal Stability Characteristics of the DOUGLAS D-558-II Research Airplane in Accelerated Maneuvers at Subsonic and Transonic Speeds

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Fischel, Jack↗

NASA NTRS1954

Longitudinal Stability and Drag Characteristics of a Fin Stabilized Body of Revolution with a Fineness Ratio of 12 as Measured by the Free-fall Method

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Kurbjun, Max C↗

NASA NTRS1954

Low-speed Longitudinal Stability and Lateral-control Characteristics of a Model of a 40 Degree Swept-wing Fighter-type Airplane at a Reynolds Number of 9 x 10(exp 6)

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Kelly, H Neale↗

NASA NTRS1954

The Effects of Changes in Aspect Ratio and Tail Height on the Longitudinal Stability Characteristics at High Subsonic Speeds of a Model with a Wing Having 32.6 Degree Sweepback

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Alford, William J , Jr↗

NASA NTRS1954

Effects of fences, leading-edge chord extensions, boundary-layer ramps, and trailing-edge flaps on the longitudinal stability of a twisted and cambered 60 degree sweptback-wing-indented-body configuration at transonic speeds

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Fischetti, Thomas L↗

NASA NTRS1954

Longitudinal Stability Characteristics in Accelerated Maneuvers at Subsonic and Transonic Speeds of the Douglas D-558-II Research Airplane Equipped with a Leading-edge Wing Chord-extension

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Fischel, Jack↗

NASA NTRS1954

Investigation of a 1/4-Scale Model of the Republic F-105 Airplane in the Langley 19-Foot Pressure Tunnel: Longitudinal Stability and Control of the Model Equipped with a Supersonic-Type Elliptical Wing-Root Inlet

No abstract available

Kelly, H Neale↗

NASA NTRS1954

Wind-tunnel Investigation at Subsonic and Supersonic Speeds of a Fighter Model Employing a Low-aspect-ratio Unswept Wing and a Horizontal Tail Mounted Well Above the Wing Plane - Longitudinal Stability and Control

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Smith, Willard G↗

NASA NTRS1954

Longitudinal Stability Characteristics at Transonic Speeds of a Canard Configuration Having a 45 Degree Sweptback Wing of Aspect Ratio 6.0 and NACA 65A009 Airfoil Section

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Vitale, A James↗

NASA NTRS1955

Longitudinal Stability Characteristics at Mach Numbers up to 0.92 of a Wing-body-tail Combination Having a Wing with 45 Degrees of Sweepback and a Tail in Various Vertical Positions

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Stephenson, Jack D↗

NASA NTRS1955

Longitudinal Stability Characteristics in Maneuvering Flight of the Convair XF-92A Delta-wing Airplane Including the Effects of Wing Fences

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Sisk, Thomas R↗