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Results for “edge”

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 973 records · Page 54

All sources NASA NTRS DOE OSTI

NASA NTRS1958

Analysis of pressure distributions for a series of tip and trailing-edge controls on a 60 deg wing at Mach numbers of 1.61 and 2.01

Supersonic pressure distributions for tip and trailing edge controls on 60 deg delta wing

TRAILING EDGE↗

NASA NTRS1966

Influence of imperfections and edge restraint on the buckling of axially compressed cylinders

Edge restraint and imperfection influence on buckling of axially compressed cylinders

BUCKLING↗

NASA NTRS1966

The effect of a fin trailing-edge wedge on the roll history of a Nike Apache

Fin trailing-edge wedge effect on Nike-Apache rocket roll history

ROLL ATTITUDE↗

NASA NTRS1966

Effect of body nose blunting, control planform area, and leading-edge bluntness on aerodynamic control of a 5 deg semivertex cone at Mach number 6.9

Effect of body nose blunting, control planform area, and leading edge bluntness on aerodynamic control of semivertex cone at hypersonic speed

HYPERSONIC SPEED↗

NASA NTRS1966

A pretensioning concept for relief of critical leading-edge thermal stress

Pretensioning technique to reduce critical operating leading-edge thermal stress in stagnation region

THERMAL STRESS↗

NASA NTRS1966

Effect of wing leading-edge shape on aerodynamic characteristics of a 67 deg swept wing-body model at Mach 1.50 to 4.63

Effect of wing leading-edge shape on aerodynamic characteristics of 67 deg swept wing-body model at Mach 1.50 to 4.63

SUPERSONIC SPEED↗

NASA NTRS1966

Influence of imperfections and edge restraint on the buckling of axially compressed cylinders.

Imperfections and edge restraint effect on buckling of axially compressed cylinders

EDGE LOADING↗

NASA NTRS1966

An exploratory study of the vortex sheets shed from the leading edges of slender wings

Analysis of vortex sheets shed from leading edges of slender wings

SLENDER WING↗

NASA NTRS1967

Stress intensity factors for crackline-loaded edge-crack specimens

Stress intensity factor for crackline loaded, edge crack flat plate specimens

STRESS↗

NASA NTRS1967

Effects of shock-wave impingement on the heat transfer on a cylindrical leading edge

Shock wave impingement effects on heat transfer on cylindrical leading edge

ROUNDED LEADING EDGE↗

NASA NTRS1967

Aerodynamic characteristics at Mach 2.03 of a series of curved-leading-edge wings employing various degrees of twist and camber

Aerodynamic characteristics at Mach 2.03 of series of curved leading edge wings employing various degrees of twist and camber

TWISTED WING↗

NASA NTRS1967

A theoretical investigation of the aerodynamics of slender wing-body combinations exhibiting leading-edge separation

Theoretical investigation of aerodynamics of slender wing-body combinations exhibiting leading edge separation

SLENDER WING↗

NASA NTRS1967

The effect of edge constraint on the buckling of sandwich and ring-stiffened 120 degree conical shells subjected to external pressure

Buckling strength of truncated conical shell at uniform external pressure on small edge

PRESSURE EFFECT↗

NASA NTRS1959

The effect of trailing-edge control deflection on the loading over a 60 deg delta-wing-body combination

Constant chord, trailing edge, control deflection effects on aerodynamic loading characteristics of 60 degree delta wing-body combination at transonic speeds

DELTA WING↗

NASA NTRS1967