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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 1,729 records · Page 96

All sources NASA NTRS DOE OSTI

NASA NTRS1959

TRANSONIC AERODYNAMIC CHARACTERISTICS OF A LATERAL CONTROL EMPLOYING ROTATABLE AIRFOILS MOUNTED VERTICALLY AT THE WING TIPS OF A 45 DEG SWEPTBACK WING, FUSELAGE, AND TAIL COMBINATION

Aerodynamic characteristics of lateral control with rotatable airfoils and sweptback wing

SWEPTBACK WING↗

NASA NTRS1963

OFF-DESIGN AERODYNAMIC CHARACTERISTICS AT MACH NUMBERS 1.61 AND 2.20 OF A SERIES OF HIGHLY SWEPT ARROW WINGS DESIGNED FOR MACH NUMBER 2.0 EMPLOYING VARIOUS DEGREES OF TWIST AND CAMBER

Off-design aerodynamic characteristics of swept arrow wings with twist and camber at supersonic velocities

OCULOGYRAL ILLUSION↗

NASA NTRS1963

AERODYNAMIC CHARACTERISTICS AT A MACH NUMBER OF 6.77 OF A 9 DEG CONE CONFIGURATION, WITH AND WITHOUT SPHERICAL AFTERBODIES, AT ANGLES OF ATTACK UP TO 180 DEG WITH VARIOUS DEGREES OF NOSE BLUNTING

Aerodynamic characteristics at mach 6.77 of 9-deg cone, with and without spherical afterbody and nose blunting at angles of attack to 180-deg

AFTERBODY↗

NASA NTRS1963

AERODYNAMIC CHARACTERISTICS OF A FLEXIBLE-CANOPY PARAGLIDER MODEL AT A MACH NUMBER OF 4.5 FOR ANGLES OF ATTACK TO 360 DEG AND SIDESLIP ANGLES FROM 0 DEG TO 90 DEG

Aerodynamic characteristics of canopy paraglider for instrument recovery - mach number, angle of attack, sideslip angle

SIDESLIP↗

NASA NTRS1963

STATIC AERODYNAMIC CHARACTERISTICS OF A THREE-STAGE ROCKET VEHICLE HAVING VARIOUS FIN CONFIGURATIONS AT LOW SUBSONIC MACH NUMBERS AND ANGLES OF ATTACK UP TO 28 DEG

Static aerodynamic characteristics of three-stage trailblazer ii rocket vehicle determined in low turbulence pressure wind tunnel

TRAILBLAZER II REENTRY VEHICLE↗

NASA NTRS1963

Effects of Nose Bluntness, Fineness Ratio, Cone Angle, and Model Base on the Static Aerodynamic Characteristics of Blunt Bodies at Mach Numbers of 1.57, 1.80, and 2.16 and Angles of Attack up to 180 Deg

Effect of nose bluntness, fineness ratio, cone angle, and model base on aerodynamic characteristics of blunt bodies

AERODYNAMIC CHARACTERISTICS↗

NASA NTRS1960

A TRANSONIC WIND-TUNNEL INVESTIGATION OF THE STATIC LONGITUDINAL AND LATERAL AERODYNAMIC CHARACTERISTICS OF A PROPOSED HYPERSONIC GLIDER WITH SEVERAL BOOSTER CONFIGURATIONS

Wind-tunnel investigation of longitudinal and lateral aerodynamic characteristics of hypersonic glider with several booster configurations

STATIC STABILITY↗

NASA NTRS1960

THE EFFECTS OF WING PLAN FORM ON THE STATIC LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF A FLAT-TOP HYPERSONIC AIRCRAFT AT MACH NUMBERS FROM 0.6 TO 1.4

Wing planform effect on static longitudinal aerodynamic characteristics of flat top hypersonic aircraft at transonic speeds

HYPERSONIC AIRCRAFT↗

NASA NTRS1963

AERODYNAMIC CHARACTERISTICS IN PITCH AT A MACH NUMBER OF 2.01 OF SEVERAL WING-BODY COMBINATIONS WITH WEDGE-SHAPED BODIES LOCATED ABOVE AND BELOW A 54.5 DEG SWEPT DELTA WING

Aerodynamic characteristics in pitch of several wing-body combinations with wedge-shaped planform located above and below a swept delta wing

DELTA WING↗

NASA NTRS1960

EFFECTS OF SPOILER-SLOT-DEFLECTOR CONTROL ON THE AERODYNAMIC CHARACTERISTICS AT A MACH NUMBER OF 2.01 OF A VARIABLE-WINGSWEEP CONFIGURATION WITH THE OUTER WING PANELS SWEPT BACK 75 DEG

Aerodynamic characteristics of variable-wing-sweep configuration with spoiler-slot-deflector control system & swept back outer wing panels

WING PANEL↗

NASA NTRS1963

TRANSONIC INVESTIGATION OF THE STATIC LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF LOW-ASPECT-RATIONWING-BODY CONFIGURATIONS AT ANGLES OF ATTACK AROM 0 DEG TO 90 DEG

Transonic wind tunnel tests for aerodynamic characteristics of wing-body configurations

TRANSONIC SPEED↗

NASA NTRS1963

A STUDY ON DYNAMIC SYSTEMS RESPONSE OF THE PERFORMANCE CHARACTERISTICS OF SOME MAJOR BIOPHYSICAL SYSTEMS

Dynamic responses of biophysical systems - performance characteristics

DYNAMIC RESPONSE↗

NASA NTRS1963

LOW-SPEED INVESTIGATION OF THE EFFECTS OF WIND SWEEP ON THE AERODYNAMIC CHARACTERISTICS OF PARAWINGS HAVING EQUAL-LENGTH LEADING EDGES AND KEEL

Low speed wind sweep effect on parawings with equal-length leading edges & keel - aerodynamic characteristics

WIND EFFECT↗

NASA NTRS1953

AERODYNAMIC CHARACTERISTICS OF LOW-ASPECT-RATIO WINGS AT HIGH SUPERSONIC MACH NUMBERS

Aerodynamic characteristics of low-aspect-ratio wings at supersonic speeds

SUPERSONIC SPEED↗

NASA NTRS1961

WIND-TUNNEL INVESTIGATION AT MACH NUMBERS FROM 0.30 TO 1.14 OF THE STATIC AERODYNAMIC CHARACTERISTICS OF MODIFIED MERCURY ESCAPE AND EXIT CAPSULE CONFIGURATIONS

Static aerodynamic characteristics of modified mercury escape and exit capsule configurations at mach numbers 0.30 to 1.4

MERCURY CAPSULE↗

NASA NTRS1961

Effects of transverse center-of-gravity displacement, afterbody geometry, and front-face curvature on the aerodynamic characteristics of Mercury-type models at a Mach number of 5.5

Effects of transverse barycenter displacement, conical afterbody, curved front face on mercury capsule supersonic aerodynamic characteristics

BARYCENTER↗

NASA NTRS1961

THE LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF A RE-ENTRY CONFIGURATION BASED ON A BLUNT 13 DEG HALF-CONE AT MACH NUMBERS TO 0.92

Longitudinal aerodynamic characteristics of blunt, lifting reentry vehicle at mach 0.92

BLUNT BODY↗

NASA NTRS1963

Comparison of Flight Measured Helicopter Rotor Blade Chordwise Pressure Distributions and Two-Dimensional Airfoil Characteristics

Helicopter rotor blade chordwise pressure distribution and two-dimensional airfoil characteristics

ROTOR BLADE↗