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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 505 records · Page 28

All sources NASA NTRS DOE OSTI

NASA NTRS1953

Comparison of the Aerodynamic Characteristics at Transonic Speeds of a Plane Wing and a Cambered and Twisted Wing, Both Having 45 Degrees of Sweepback and an Aspect Ratio of 6

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Holdaway, George H↗

NASA NTRS1953

Measurements of fluctuating pressures on the wings and body of a sweptback wing-body combination in the Langley 16-foot transonic tunnel

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Habel, Louis W↗

NASA NTRS1953

Wind-tunnel Investigation of the Vortex Wake and Downwash Field Behind Triangular Wings and Wing-body Combinations at Supersonic Speeds

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Spahr, J Richard↗

NASA NTRS1953

An Analysis of the Tracking Performances of Two Straight-wing and Two Swept-wing Fighter Airplanes with Fixed Sights in a Standardized Test Maneuver

Standard air-to-air-gunnery tracking runs were conducted with F-51H, F8F-1, F-86A, and F-86E airplanes equipped with fixed gunsights. The tracking performances were documented over the normal operating range of altitude, Mach number, and normal acceleration factor for each airplane. The sources of error were studied by statistical analyses of the aim wander.

CONTROL, LATERAL↗

NASA NTRS1952

Aerodynamic characteristics at supersonic speeds of a series of wing-body combinations having cambered wings with an aspect ratio of 3.5 and a taper ratio of 0.2 : effects of sweep angle and thickness ratio on the static lateral stability characteris

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Hilton, John H , Jr↗

NASA NTRS1952

Free-flight Measurements of Some Effects of Aileron Span, Chord, and Deflection and of Wing Flexibility on the Rolling Effectiveness of Ailerons on Sweptback Wings at Mach Numbers Between 0.8 and 1.6

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Strass, H Kurt↗

NASA NTRS1952

Aerodynamic Characteristics at Supersonic Speeds of a Series of Wing-body Combinations Having Cambered Wings with an Aspect Ratio of 3.5 and a Taper Ratio of 0.2 : Effects of Sweep Angle and Thickness Ratio on the Aerodynamic Characteristics in Pitch

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Driver, Cornelius↗

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 NTRS1953

Wind-tunnel investigation at low speed of the effect of varying the ratio of body diameter to wing span from 0.1 to 0.8 on the aerodynamic characteristics in pitch of a 45 degree sweptback-wing-body combination

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Johnson, Harold S↗

NASA NTRS1952

Investigation of the Distribution of Lift, Drag, and Pitching Moment Between the Wing and Fuselage of a 1/30-scale Semispan Model of the Bell X-5 Airplane at a Mach Number of 1.24 by the Naca Wing-flow Method

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Morris, Garland J↗

NASA NTRS1954

Wind-tunnel investigation at high subsonic speeds to determine the rolling derivatives of two wing-fuselage combinations having triangular wings, including a semiempirical method of estimating the rolling derivatives

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Wiggins, James W↗

NASA NTRS1952

Lift, Drag, and Pitching Moment of Low-aspect-ratio Wings at Subsonic and Supersonic Speeds : an Investigation at Large Reynolds Numbers of the Low-speed Characteristics of Several Wing-body Combinations

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Smith, Donald W↗

NASA NTRS1954

Flight Investigation of Engine Nacelles and Wing Vertical Position on the Drag of a Delta-wing Airplane Configuration Form Mach Number 0.8 to 2.0

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Judd, Joseph 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

Effects of Operating Propellers on the Wing-surface Pressures of a Four-engine Tractor Airplane Configuration Having a Wing with 40 Degrees of Sweepback

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Boltz, Frederick W↗

NASA NTRS1954

Summary of Some Rocket-model Investigations of Effects of Wing Aspect Ratio and Thickness on Aileron Rolling Effectiveness Including Some Effects of Spanwise Aileron Location for Sweptback Wings with Aspect Ratio of 8.0

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Strass, H Kurt↗

NASA NTRS1954

Aerodynamic characteristics of a cruciform-wing missile with canard control surfaces and of some very small span wing-body missiles at a Mach number of 1.41

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Spearman, M Leroy↗

NASA NTRS1954

Investigation at High Subsonic Speeds of Finned and Unfinned Bodies Mounted at Various Locations from the Wings of Unswept- and Swept-wing--fuselage Models, Including Measurements of Body Loads

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Silvers, H Norman↗