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Results for “TiP”

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 1,045 records · Page 58

All sources NASA NTRS DOE OSTI

NASA NTRS1952

Investigation of turbines suitable for use in a turbojet engine with high compressor pressure ratio and low compressor tip-speed II : velocity-diagram study of turbine for engine operation with constant exhaust-nozzle area

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Davison, Elmer H↗

NASA NTRS1952

Investigation of turbines suitable for use in a turbojet engine with high compressor pressure ratio and low compressor-tip speed III : velocity-diagram study of two-stage and downstream-stator turbines for engine operation at constant rotative speed

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English, Robert E↗

NASA NTRS1952

Rocket-model Investigation to Determine the Force and Hinge-moment Characteristics of a Half-delta Tip Control on a 59 Degree Sweptback Delta Wing Between Mach Numbers of 0.55 and 1.43

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Martz, C William↗

NASA NTRS1952

Investigation of turbines suitable for use in a turbojet engine with high compressor pressure ratio and low compressor-tip speed IV : effect of increasing blade speed on velocity diagrams of turbine for engine operation at constant rotative speed

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Davison, Elmer H↗

NASA NTRS1952

Control Hinge-moment and Effectiveness Characteristics of a 60 Degree Half-delta Tip Control on a 60 Degree Delta Wing at Mach Numbers of 1.41 and 1.96

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Guy, Lawrence D↗

NASA NTRS1952

The Longitudinal Stability and Control Characteristics of a 60 Degree Delta-wing Missile Having Half-delta Tip Controls as Obtained from a Free-flight Investigation at Transonic and Supersonic Speeds

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Moul, Martin T↗

NASA NTRS1953

Hinge-moment Characteristics for Several Tip Controls on a 60 Degree Sweptback Delta Wing at Mach Number 1.61

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Czarnecki, K R↗

NASA NTRS1953

An Experimental Investigation of the Effect of Various Parameters Including Tip Mach Number on the Flutter of Some Model Helicopter Rotor Blades

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Brooks, George W↗

NASA NTRS1952

The Effects of Tip-mounted Jet Nacelles on the Transonic Characteristics of Low-aspect-ratio Wings

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Coe, Charles F↗

NASA NTRS1953

A method for calculating the aerodynamic loading on wing-tip-tank combinations in subsonic flow

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Robinson, Samuel W , Jr↗

NASA NTRS1953

Some flutter experiments at a Mach number of 1.3 on cantilever wings with tubular and closed bodies at the tips

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Mccarty, John Locke↗

NASA NTRS1953

Experimental Investigation of an Axial-flow Compressor Inlet Stage Operating at Transonic Relative Inlet Mach Numbers III : Blade-row Performance of Stage with Transonic Rotor and Subsonic Stator at Corrected Tip Speeds of 800 and 1000 Feet Per Secon

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Schwenk, Francis C↗

NASA NTRS1953

Low-speed investigation of the lateral control characteristics of three tip ailerons on a 60 degree triangular wing

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Gottlieb, Stanley M↗

NASA NTRS1953

Effect of Reduction in Thickness from 6 to 2 Percent and Removal of the Pointed Tips on the Subsonic Static Longitudinal Stability Characteristics of a 60 Degree Triangular Wing in Combination with a Fuselage

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Palmer, William E↗

NASA NTRS1953

Preliminary Investigation of the Effect of Fences and Balancing Tabs on the Hinge-moment Characteristics of a Tip Control on a 60 Degree Delta Wing at Mach Number 1.61

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Czarnecki, K R↗

NASA NTRS1953

Recent information on flap and tip controls

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Lord, Douglas R↗

NASA NTRS1953

Control hinge-moment and effectiveness characteristics of several interchangeable tip controls on a 60 degree delta wing at Mach numbers of 1.41, 1.62, and 1.96

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Morris, Odell A↗

NASA NTRS1953

Effect of large deflection of a canard control and deflections of a wing-tip control on the static-stability and induced-roll characteristics of a cruciform canard missile at a Mach number of 2.01

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Spearman, M Leroy↗