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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

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 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Performance of External internal Compression Inlet with Abrupt Internal Turning at Mach Numbers 3 0 to 2 0

Download or read book Performance of External internal Compression Inlet with Abrupt Internal Turning at Mach Numbers 3 0 to 2 0 written by Leonard J. Obery and published by . This book was released on 1957 with total page 21 pages. Available in PDF, EPUB and Kindle. Book excerpt: An inlet with combined external and internal compression, formed by spike and cowl oblique shocks, and an over-all length of 2.5 inlet diameters was investigated at Mach numbers from 3.0 to 2.0 over a range of angles of attack. At the design Mach number of 3.0 the low angle cowl, which turned the flow supersonically, generated two internal shocks and focused them on the centerbody surface. These compression waves, with their high pressure gradient, were cancelled by abrupt centerbody turning. This investigation showed that with proper boundary-layer control on the centerbody this method of internal compression did not adversely affect the high performance of the inlet.

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

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:

Book Performance of an Axisymmetric External compression and a Two dimensional External internal compression Inlet at Mach 4 95

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:

Book Index to NASA Technical Publications

Download or read book Index to NASA Technical Publications written by United States. National Aeronautics and Space Administration and published by . This book was released on 1960-07 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Investigation of an Underslung Half cone Inlet with Compression Surface Mounted Outboard from Fuselage at Mach Numbers of 1 5 1 8 and 2 0

Download or read book Investigation of an Underslung Half cone Inlet with Compression Surface Mounted Outboard from Fuselage at Mach Numbers of 1 5 1 8 and 2 0 written by Richard A. Yeager and published by . This book was released on 1958 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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

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:

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

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:

Book Performance Characteristics at Mach Numbers to 2 0 of Various Types of Side Inlets Mounted on Fuselage of Proposed Supersonic Airplane

Download or read book Performance Characteristics at Mach Numbers to 2 0 of Various Types of Side Inlets Mounted on Fuselage of Proposed Supersonic Airplane written by Paul C. Simon and published by . This book was released on 1952 with total page 35 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Performance of a Mach Number 3 0 Design Axisymmetric Double cone External compression Inlet in Mach Number Range 2 07 to 1 48

Download or read book Performance of a Mach Number 3 0 Design Axisymmetric Double cone External compression Inlet in Mach Number Range 2 07 to 1 48 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:

Book Internal Performance of Several Auxiliary Air Inlets Immersed in a Turbulent Boundary Layer at Mach Numbers of 1 3 1 5 and 2 0

Download or read book Internal Performance of Several Auxiliary Air Inlets Immersed in a Turbulent Boundary Layer at Mach Numbers of 1 3 1 5 and 2 0 written by Ronald G. Huff and published by . This book was released on 1957 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt: Internal performance of normal-shock rectangular, circular, and scoop inlets and of external-compression inlets experimentally obtained with varying immersion in a turbulent boundary layer. Recoveries varied from about 95 percent of theoretical in the free stream to 80 percent with complete immersion, while the corresponding mass flows were usually above 95 percent of theoretical. Turning of the flow through 10 degrees caused losses in pressure recovery of 0.03 to 0.07. External compression did not improve pressure recovery in the boundary layer. Average distortion at critical operation for all inlets was 5 percent.