Comparison of test results from a 90 deg sector and a full annulus advanced turbojet combustor
Separate component test rigs for 90 degree sector combustor and full annular turbojet combustor comparison
Perkins, P. J.↗
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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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THEMIS signal analysis statistics research program - Development and analysis of modified paired comparisons by use of linearized nonlinear regression
Curve fitting for modified paired comparisons using linearized nonlinear regression
Walsh, J. E.↗
Comparison of solar-electric propulsion systems for the synchronous equatorial satellite-raising mission
Comparison of solar electric propulsion systems for synchronous equatorial satellite-raising mission
Hrach, F. J.↗
Comparison of Flaw Growth Characteristics Under Cryogenic Proof and Ambient Test Conditions for Apollo Titanium Pressure Vessels
Comparison of flaw growth characteristics under cryogenic proof and ambient test conditions for Apollo titanium pressure vessels
Bixler, W. D.↗
Data from falling sphere experiments including comparison tests between different systems
Data comparison for falling sphere experimental measurements on atmospheric density
Smith, L. B.↗
Check of a three-dimensional reactor shielding code by comparison with ML-1 reactor experiment
Three dimensional Monte Carlo reactor shielding code evaluation by comparison with dose rate measurement on reactor shield assembly
Schamberger, R. D.↗
A latitude comparison of N2 density measurements by mass spectrometer
Latitude comparison of N2 ion density measurement by experimental mass spectrometer
Schaefer, E. J.↗
Free flight investigation of large all- flexible parawings and performance comparison with small parawings Final report
Free flight investigation of large all-flexible parawings and performance comparison with small parawings to provide land-landing capability for manned spacecraft
Gran, W. M.↗
Applications of variable property heat- transfer and friction equations to rocket nozzle coolant passages and comparison with nuclear rocket test results
Variable property heat transfer and friction equations to rocket nozzle coolant passages and comparison with nuclear rocket test results
Taylor, M. F.↗
Comparison of flame spreading over thin flat surfaces in normal gravity and weightlessness in an oxygen environment
Comparison of flame spreading over thin flat surfaces in normal gravity and weightlessness in oxygen environment
Andracchio, C. R.↗
Numerical error comparisons for integration of near earth orbits in various coordinate systems
Numerical error comparisons for integration of near earth orbits in various coordinate systems
Schwausch, O. A.↗
A comparison of the Fano and Jelinek sequential decoding algorithms
Comparison of Fano and Jelinek sequential decoding algorithms
Geist, J. M.↗
Flight comparison of several techniques for determining the minimum flying speed for a large, subsonic jet transport
Flight comparison of techniques for determining minimum flying speed for large, subsonic jet transport
Kier, D. A.↗
Comparison and correlation of experimental results
Empirical evaluation and comparison of test data for mass-loaded and unloaded shells
Source record↗
XB-70 flight test data comparisons with simulation predictions of inlet unstart and buzz
XB-70 flight test data comparison with simulated predictions of inlet unstart and buzz
Beaulieu, W. D.↗
Comparison of a modified Kjeldahl and vacuum fusion techniques for determination of nitrogen in tantalum alloys
Comparison of nitrogen determination in tantalum alloys by Kjeldahl and vacuum fusion techniques
Davis, W. F.↗
Comparison of cord loads with a 24 x 7.7 type 7 aircraft tire on grooved and smooth runway surfaces
Comparison of cord loads with aircraft tire on grooved and smooth runway surfaces
Clark, S. K.↗
A comparison between experimental data and a lifting surface theory calculation of vortex induced loads
Comparison between experimental data and lifting surface theory calculation of vortex induced loads on single-bladed rotary wings
Johnson, W.↗