Nonlinear effects in bounded compressible plasmas excited by external sources.
Nonlinear effects in bounded compressible plasmas excited by external sources
Paik, S. F.↗
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Effects of thermal compression on the performance estimates of hypersonic ramjets.
Thermal compression effects on hypersonic ramjets performance, discussing thermodynamic cycle calculation based on gas dynamic model
Billig, F. S.↗
Experimental investigation of sandwich cylinders and cones subjected to axial compression.
Sandwich cylinders and cones axial compression general instability buckling loads
Baker, E. H.↗
Admittance of an inhomogeneously sheathed infinite cylindrical antenna immersed in an isotropic, compressible plasma.
Admittance of inhomogeneously sheathed infinite cylindrical antenna immersed in istropic compressible plasma
Miller, E. K.↗
Information rates for data compression.
Upper and lower bounds on required information rate for data compression fidelity criterion, comparing bounds with equivalent mean-square-error result
Davisson, L. D.↗
A method for the analysis of halocarbon oil contamination in compressed gases
Gas chromatographic-electron capture system for analysis of halocarbon oil contamination in compressed gases
Carlin, F. J., Jr.↗
Compressive properties and column efficiency of metals reinforced on the surface with bonded filaments
Compressive properties and weight saving of metals reinforced on surface with resin bonded fibers
Dexter, H. B.↗
Preliminary investigation of distortion dynamics in a Mach 3 mixed compression inlet
Wind tunnel tests of distortion dynamics in Mach three mixed compression inlet
Coltrin, R. E.↗
Theory for computing span loads and stability derivatives due to sideslip, yawing, and rolling for wings in subsonic compressible flow
Computing span loads and stability derivatives due to sideslip, yawing, and rolling for wings in compressible flow
Queijo, M. J.↗
Effect of bleed-system back pressure and porous area on the performance of an axisymmetric mixed-compression inlet at Mach 2.50
Performance tests of wind tunnel model inlet for bleed system back pressure and porous area effect of axisymmetric compression
Cubbison, R. W.↗
The general instability of eccentrically stiffened cylindrical shells under axial compression and lateral pressure
Instability of eccentrically stiffened cylindrical shells under axial compression and lateral pressure
Brolliar, R. H.↗
Time and Source Encoding for Multiplexed Compressed Signals
Time and source encoding for multiplexed compressed telemetry signals
Broglio, C. J.↗
Design and performance of flueric shock position sensor for a mixed-compression supersonic inlet
Design and performance of flueric shock position sensor for mixed compression supersonic inlets
Griffin, W. S.↗
Performance characteristics from Mach 2.58 to 1.98 of an axisymmetric mixed-compression inlet system with 60-percent internal contraction
Performance test from Mach 2.58 to 1.98 of axisymmetric mixed-compression inlet system with 60 percent internal contraction
Cubbison, R. W.↗
Characteristics study of a bicone mixed- compression inlet for Mach 1.80 to 2.50
Characteristics study of bicone mixed compression inlet for Mach 1.80 to 2.50
Anderson, B. H.↗
Calculation of compressible turbulent boundary layers with pressure gradients and heat transfer
Calculation of compressible turbulent boundary layers with pressure gradients and heat transfer
Kuhn, G. D.↗
Restart and high response terminal shock control for an axisymmetric mixed-compression inlet with 60-percent internal contraction
Restart and high response terminal shock control for axisymmetric mixed-compression inlet with internal contraction
Cole, G. L.↗
Compressed Gas Handbook
High pressure compressible flow systems in space vehicle ground support equipment
Cota, R. A.↗