Download or read book Experimental Investigation of a 2 D Scramjet Inlet at Mach Numbers of 8 18 and Stagnation Temperatures of 4 100K written by M. Minucci and published by . This book was released on 1991 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book An Experimental Investigation of a 2 D Scramjet Inlet at Flow Mach Numbers of 8 to 25 and Stagnation Temperatures of 800 to 4 100K written by Marco Antonio Sala Minucci and published by . This book was released on 1991 with total page 339 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Experimental Investigation of a 3 D Scramjet Inlet for Laser Propulsion at Mach Numbers of 8 to 18 and a Stagnation Temperature of 4 100 K written by R. A. Jones and published by . This book was released on 1991 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Experimental Investigation of a 3 D Scramjet Inlet for Laser Propulsion at Mach Numbers of 8 to 18 and a Stagnation Temperature of 4100 K written by R. A. Jones and published by . This book was released on 1991 with total page 10 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Experimental Investigation of a 3 D Scramjet Inlet for Laser Propulsion at Mach Numbers of 10 to 25 and Stagnation Temperatures of 800 to 4100 Degrees K written by R. A. Jones and published by . This book was released on 1991 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Computational and Experimental Investigation of a 2 D Scramjet Inlet at Mach Numbers from 10 to 25 written by D. Messitt and published by . This book was released on 1993 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Combined Numerical and Experimental Investigation of a 2 D Scramjet Inlet at Mach Numbers 10 to 25 written by D. G. Messitt and published by . This book was released on 1995 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Experimental Investigation of Generic Three dimensional Sidewall compression Scramjet Inlets at Mach 6 in Tetrafluoromethane written by Scott D. Holland and published by . This book was released on 1993 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Experimental Investigation of a Large scale Two dimensional Mixed compression Inlet System written by Norman D. Wong and published by . This book was released on 1971 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt: A large-scale, variable-geometry inlet model with a design Mach number of 3.0 was tested at Mach numbers from 1.55 to 3.2. Variable features of the inlet for off-design operation are an adjustable-height ramp system and a translating cowl. This report presents experimental results for a diffuser and boundary-layer bleed configuration which was optimized at the design Mach number. Overall performance was high with throat-mounted vortex generators, which were effective in reducing flow distortion in the subsonic diffuser at the higher Mach numbers.
Download or read book An Experimental Investigation at Mach Numbers from 2 1 to 3 0 of Circular Internal compression Inlets Having Translatable Centerbodies and Provisions for Boundary layer Removal written by Earl C. Watson and published by . This book was released on 1960 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Experimental Investigation of a Mach 5 Isentropic Spike Inlet at and Below Design Speed written by Leonard E. Stitt and published by . This book was released on 1959 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Experimental Investigation of Inlet Combustor Isolators for a Dual Mode Scramjet at a Mach Number of 4 written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-06 with total page 96 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report details experimentally derived operational characteristics of numerous two-dimensional planar inlet-combustor isolator configurations at a Mach number of 4. Variations in geometry included (1) inlet cowl length; (2) inlet cowl rotation angle; (3) isolator length; and (4) utilization of a rearward-facing isolator step. To obtain inlet-isolator maximum pressure-rise data relevant to ramjet-engine combustion operation, configurations were mechanically back pressured. Results demonstrated that the combined inlet-isolator maximum back-pressure capability increases as a function of isolator length and contraction ratio, and that the initiation of unstart is nearly independent of inlet cowl length, inlet cowl contraction ratio, and mass capture. Additionally, data are presented quantifying the initiation of inlet unstarts and the corresponding unstart pressure levels. Emami, Saied and Trexler, Carl A. and Auslender, Aaron H. and Weidner, John P. Langley Research Center...
Download or read book Experimental Study of a Two dimensional Scramjet at Mach Numbers of 8 to 25 written by M. A. S. Minnuci and published by . This book was released on 1990 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Reynolds Number and Cowl Position Effects for a Generic Sidewall Compression Scramjet Inlet at Mach 10 written by Scott D. Holland and published by . This book was released on 1992 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Mach 10 Computational Study of a Three Dimensional Scramjet Inlet Flow Field written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-05 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: The present work documents the computational results for a combined computational and experimental parametric study of the internal aerodynamics of a generic three-dimensional sidewall-compression scramjet inlet configuration at Mach 10. The three-dimensional Navier-Stokes code SCRAMIN was chosen for the computational portion of the study because it uses a well-known and well-proven numerical scheme and has shown favorable comparison with experiment at Mach numbers between 2 and 6. One advantage of CFD was that it provided flow field data for a detailed examination of the internal flow characteristics in addition to the surface properties. The experimental test matrix at mach 10 included three geometric contraction ratios (3, 5, and 9), three Reynolds numbers (0.55 x 10(exp 6) per foot, 1.14 x 10(exp 6) per foot, and 2.15 x 10(exp 6) per foot), and three cowl positions (at the throat and two forward positions). Computational data for two of these configurations (the contraction ratio of 3, Re = 2.15 x 10 (exp 6) per foot, at two cowl positions) are presented along with a detailed analysis of the flow interactions in successive computational planes. Holland, Scott D. Langley Research Center RTOP 506-40-41-02...
Download or read book Experimental Investigation of a 3 D Flow Field for an External MHD Propulsor at Mach Numbers of 10 to 25 and a Stagnation Temperature of 1200 K written by Paul C. Dallemagne and published by . This book was released on 1992 with total page 69 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Performance of External compression Bump Inlet at Mach Numbers of 1 5 to 2 0 written by Paul C. Simon and published by . This book was released on 1957 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:
