• Organization: National Aeronautics and Space Administration
• Updated: 2025-07-17

Shock Wave / Turbulent Boundary Layer Flows at High Mach Numbers. This web page provides data from experiments that may be useful for the validation of turbulence models. This resource is expected...

• Organization: National Aeronautics and Space Administration
• Updated: 2025-07-17

Shock Wave / Turbulent Boundary Layer Flows at High Mach Numbers. This web page provides data from experiments that may be useful for the validation of turbulence models. This resource is expected...

• Organization: National Aeronautics and Space Administration
• Updated: 2025-07-17

Shock Wave / Turbulent Boundary Layer Flows at High Mach Numbers. This web page provides data from experiments that may be useful for the validation of turbulence models. This resource is expected...

• Organization: National Aeronautics and Space Administration
• Updated: 2025-07-17

Shock Wave / Turbulent Boundary Layer Flows at High Mach Numbers. This web page provides data from experiments that may be useful for the validation of turbulence models. This resource is expected...

• Organization: National Aeronautics and Space Administration
• Updated: 2025-07-17

Shock Wave / Turbulent Boundary Layer Flows at High Mach Numbers. This web page provides data from experiments that may be useful for the validation of turbulence models. This resource is expected...

• Organization: National Aeronautics and Space Administration
• Updated: 2025-04-23

Wall pressure data acquired during flight tests at three flight conditions are provided: 48k feet altitude at Mach 0.86; 32k feet at Mach 0.70; and 24k feet at Mach 0.56. Details of the flight...

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• Organization: National Aeronautics and Space Administration
• Updated: 2025-03-31

This is a textbook, created example for illustration purposes. The System takes inputs of Pt, Ps, and Alt, and calculates the Mach number using the Rayleigh Pitot Tube equation if the plane is...

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• Organization: National Aeronautics and Space Administration
• Updated: 2025-03-31

This is the bird of the skies of the future. The heavy lift cargo aircraft which is currently being developed by me has twice the payload capacity of an Antonov A-225 aircraft and in hypersonic...

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• Organization: National Aeronautics and Space Administration
• Updated: 2025-03-31

The databases of computational and experimental data from the first Aeroelastic Prediction Workshop are located here. The databases file names tell their contents by configuration, angle of...

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• Organization: Department of the Interior
• Updated: 2020-10-16T00:00:00Z

This dataset includes skin temperatures of twelve Tadarida brasiliensis held in environmental chambers maintained at 7.7 (SD 0.9) °C and 91.8 (SD 0.8) % relative humidity to induce and support...

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• Organization: National Aeronautics and Space Administration
• Updated: 2025-07-17

This data set contains the best estimates of the total ion density from Voyager 2 at Jupiter in the PLS voltage range (10-5950 eV/Q). It is calculated using the method of which to first order...

• Organization: National Aeronautics and Space Administration
• Updated: 2025-07-17

THIS DATA SET CONTAINS THE BEST ESTIMATES OF THE TOTAL ION DENSITY FROM VOYAGER 2 AT JUPITER IN THE PLS VOLTAGE RANGE (10-5950 EV/Q). IT IS CALCULATED USING THE METHOD OF MCNUTT ET AL. (1981)...

• Organization: National Aeronautics and Space Administration
• Updated: 2025-07-17

THIS DATA SET CONTAINS THE BEST ESTIMATES OF THE TOTAL ION DENSITY FROM VOYAGER 2 AT JUPITER IN THE PLS VOLTAGE RANGE (10-5950 EV/Q). IT IS CALCULATED USING THE METHOD OF MCNUTT ET AL. (1981)...

• Organization: National Institute of Standards and Technology
• Updated: 2024-05-28 00:00:00

Theoretical calculation, simulation and experimental measurement data from the paper "Bound-state-in-continuum guided modes in a multilayer electro-optically active photonic integrated circuit...

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• Organization: National Aeronautics and Space Administration
• Updated: 2025-07-17

THIS DATA SET CONTAINS THE BEST ESTIMATES OF THE TOTAL ION DENSITY AT JUPITER DURING THE VOYAGER 1 ENCOUNTER IN THE PLS VOLTAGE RANGE (10-5950 EV/Q). IT IS CALCULATED USING THE METHOD OF MCNUTT ET...

• Organization: National Aeronautics and Space Administration
• Updated: 2025-07-17

THIS DATA SET CONTAINS THE BEST ESTIMATES OF THE TOTAL ION DENSITY AT JUPITER DURING THE VOYAGER 1 ENCOUNTER IN THE PLS VOLTAGE RANGE (10-5950 EV/Q). IT IS CALCULATED USING THE METHOD OF MCNUTT ET...

• Organization: National Institute of Standards and Technology
• Updated: 2022-04-26 00:00:00

Data for all measurements published in the manuscript "Bipolar Waveform Synthesis with an Optically Driven Josephson Arbitrary Waveform Synthesizer," which will be published in the journal "IEEE...

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• Organization: Department of Energy
• Updated: 2024-01-02T18:23:19Z

This dataset contains aerodynamic quantities - including flow field values (momentum, energy, and vorticity) and summary values (coefficients of lift, drag, and momentum) - for 8,996 airfoil...

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• Organization: Department of Energy
• Updated: 2024-01-02T18:21:46Z

This dataset contains aerodynamic quantities - including flow field values (momentum, energy, and vorticity) and summary values (coefficients of lift, drag, and momentum) - for 1,830 airfoil...

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• Organization: National Aeronautics and Space Administration
• Updated: 2026-02-10

FIRE_CI2_CITATN_5SEC data are First ISCCP (International Satellite Cloud Climatology Project) Regional Experiment (FIRE) Cirrus 2 University of North Dakota Citation Aircraft 5 Second Data in...

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