Download or read book Performance of an Axisymmetric External compression and a Two dimensional External internal compression Inlet at Mach 4 95 written by James F. Connors and published by . This book was released on 1959 with total page 19 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Performance Characteristics of a Wing body Combination with a Two dimensional External internal compression Inlet at Mach 3 5 and 3 0 written by and published by . This book was released on 1960 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Performance of a Mach Number 3 0 Design Axisymmetric Double cone External compression Inlet in the Mach Number Range 1 97 to 0 79 written by Owen H. Davis and published by . This book was released on 1960 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Procedures for Estimating Inlet External and Internal Performance written by B. M. Sharp and published by . This book was released on 1974 with total page 284 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Performance of a Mach 3 0 External internal Compression Axisymmetric Inlet at Mach Numbers from 2 0 to 3 5 written by and published by . This book was released on 1960 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Performance Summary and Analysis of a Mach 3 0 Design Axisymmetric All external compression Double cone Inlet Mach Number Range 3 0 to 0 8 written by John L. Allen and published by . This book was released on 1960 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Investigation of the Performance and Control of a Mach 3 0 Two dimensional External internal compression Inlet written by and published by . This book was released on 1961 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effect of External Boundary Layer on Performance of Axisymmetric Inlet at Mach Numbers of 3 0 and 2 5 written by N. E. Samanich 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 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:
Download or read book Zero angle of attack Performance of Two dimensional Inlets Near Mach Number 3 written by Richard R. Woollett and published by . This book was released on 1956 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: An extensive program was undertaken to investigate the effect of several geometric variables on the performance of two-dimensional inlets. This investigation included inlets having single-wedge, double-wedge, and isentropic compression ramps with various side-plate configurations and subsonic diffusers. The tests were conducted over a range of Reynolds number based on inlet height from 0.50 to 2.67(sup x)10(sup 6). Generally, the performance levels of the two-dimensional inlets were somewhat below those obtained previously with comparable axisymmetric models. At Mach number 3.05 the optimum total-pressure recovery was obtained with an isentropic inlet which compressed the external flow to a Mach number of 1.88. Rectangular side plates and a long high-exit-Mach-number subsonic diffuser with filleted corners were used with this inlet. A critical total-pressure recovery of 0.71 was realized with a corresponding mass-flow ratio of 0.965. Subcritical stability to a mass-flow ratio of 0.60 was obtained.
Download or read book A Comparison of the Performance of Four Side mounted Inlets Over a Mach Number Range of 0 88 to 2 2 and Angles of Attack to 14 written by Leroy L. Presley and published by . This book was released on 1960 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Memorandum written by and published by . This book was released on 1963 with total page 200 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Performance of Mach No 3 0 Design Axisymmetric Double cone External compression Inlet in Mach Number Range 2 07 to 1 48 with List of References written by John L. Allen and published by . This book was released on 1959 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book PERFORMANCE SUMMARY AND ANALYSIS OF A MACH 3 0 DESIGN AXISYMMETRIC ALL EXTERNAL COMPRESSION DOUBLE CONE INLET FROM MACH NUMBER 3 0 TO 0 8 written by and published by . This book was released on 1960 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Investigation of Three Mach 7 External Compression Axisymmetric Inlets from Mach 1 9 to 6 8 written by and published by . This book was released on 1960 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Performance of Three Isentropic All Internal Compression Axisymmetric Inlets Designed for Mach 2 5 written by Bernhard H. Anderson 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 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.
