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Results for “model scaling”

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 649 records · Page 36

All sources NASA NTRS DOE OSTI

DOE OSTI2026

Predicting metal plasticity through cross-scale modeling

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Materials science↗

NASA NTRS1960

Pressure Distribution of a 0.0667-Scale Model of the X-15 Airplane for an Angle-Of-Attack Range of 0 deg To 28 deg at Mach Numbers of 2.30, 2.88, and 4.65

Pressure distribution on x-15 aircraft model

PRESSURE DISTRIBUTION↗

NASA NTRS1959

WIND-TUNNEL INVESTIGATION OF THE STATIC STABILITY OF A 1 56-SCALE MODEL OF THE X-1E AIRPLANE AT MACH NUMBERS OF 2.37, 2.98, AND 4.01

Wind tunnel tests of static stability of model x-1e aircraft at mach 2 to 4

X-1 AIRCRAFT↗

NASA NTRS1960

FIN LOADS AND TIP-CONTROL HINGE MOMENTS ON A 1 8-SCALE MODEL SIMULATING THE FIRST STAGE OF THE SCOUT RESEARCH VEHICLE AT A MACH NUMBER OF 2.01

Supersonic wind tunnel testing - scout vehicle fin load and tip control hinge moments

TIP CONTROL↗

NASA NTRS1952

FREE-SPINNING-TUNNEL INVESTIGATION OF A 1 30-SCALE MODEL OF THE GRUMMAN XS2F-1 AIRPLANE

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Healy, F. M.↗

NASA NTRS1964

Experimental lateral vibration characteristics of a one fifth-scale model of saturn sa-1 with an eight-cable suspension system

Resonant frequencies, mode shapes, and vibrational damping characteristics of Saturn S- I stage model

SUSPENSION SYSTEM↗

NASA NTRS1959

Transonic and supersonic ejection release characteristics of six dynamically scaled external-store shapes from an 0.086-scale model of a current fighter airplane

Fighter aircraft external stores ejection at transonic and supersonic speeds

EJECTION↗

NASA NTRS1966

Cold-air performance evaluation of scale model oxidizer pump-drive turbine for the M-1 hydrogen-oxygen rocket engine. II - Overall two-stage performance

Cold flow test of pump drive turbines for M-1 rocket engine

M-1 ROCKET ENGINE↗

NASA NTRS1961

Investigation of the subsonic and supersonic release characteristics of an externally carried fuel tank from a 1/4 d-scale model of a bomber airplane

Release and flight characteristics study for externally carried fuel tank models of various configurations at subsonic and supersonic speeds

FLIGHT CHARACTERISTICS↗

NASA NTRS1960

Effects of vertical-tail size and a ventral fin on the static lateral and directional stability derivatives of a 0.048-scale model of a horizontal-attitude VTOL airplane at transonic speeds

Vertical tail size and ventral fin effects on lateral and directional stability of VTOL AIRCRAFT at transonic speeds

VTOL AIRCRAFT↗

NASA NTRS1960

Aerodynamic characteristics in pitch, including effects of horizontal-tail negative dihedral angle, of a 0.048-scale model of a horizontal-attitude VTOL airplane at transonic speeds

Aerodynamic characteristics in pitch of horizontal attitude VTOL aircraft, including effects of negative dihedral horizontal tail

PITCHING MOMENT↗

NASA NTRS1966

Low-speed tests of 50 deg-swept parawings applied to a 0.17-scale model of a manned flight vehicle

Shock wave interference and degradation in wind tunnel caused by protruding teeth, recessions, local expansions, and combinations of these

SWEPT WING↗

NASA NTRS1966

Hypersonic static stability investigation of a Tomahawk 20-percent-scale model Technical report, 27 May - 2 Jun. 1966

Hypersonic static stability investigation of Tomahawk rocket model

HYPERSONIC FLOW↗

NASA NTRS1968

Scale model study of flow patterns in the inlet manifold of the fuel pump drive turbine for the M-1 hydrogen-oxygen rocket engine

Flow conditions in inlet manifold of M-1 fuel pump drive turbine investigated using circumferential static pressure measurements in conjunction with smoke trace photographs

Kline, J. F.↗

NASA NTRS1968