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EBookClubs

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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 Experimental Evaluation of Inlet Drag Characteristics in the Transonic Mach Number Regime

Download or read book Experimental Evaluation of Inlet Drag Characteristics in the Transonic Mach Number Regime written by Francis D. McVey and published by . This book was released on 1968 with total page 692 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report presents the results of a test program to determine the drag of supersonic inlets operating at transonic Mach number conditions. It is a supplement to Air Force Report AFAPL-TR-68-119 describing the results of additional tests conducted under Air Force Contract F33615-68-C-1520. Data are presented showing the additive drag and total inlet drag of the F-4 aircraft inlet measured in the presence of the aircraft forebody and in an undisturbed stream. Inlet drag test data are also presented for a series of thirteen configurations where the sideplate geometry is the primary variable. All thirteen configurations are variations on a single two-dimensional inlet. Tests to reproduce some of the data reported in AFAPL-TR-68-119 were conducted to evaluate the accuracy of the experimental procedure. (Author).

Book NASA Technical Memorandum

Download or read book NASA Technical Memorandum written by and published by . This book was released on 1980 with total page 104 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Investigation of Methods for the Structural Weight Analysis of a Mach 2 4 Axisymmetric Inlet

Download or read book Investigation of Methods for the Structural Weight Analysis of a Mach 2 4 Axisymmetric Inlet written by National Aeronautics and Space Adm Nasa and published by . This book was released on 2018-10-20 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: Structural design and analysis tools appropriate for estimating the structural weight of an axisymmetric inlet designed for Mach 2.4 cruise were evaluated. Little information regarding the inlet mechanical design is available in the preliminary design phase, so it is necessary to first develop a reasonable structural design before estimating the inlet weight. The Internally Pressurized Structure Synthesis and Optimization (IPSSO) program, employing an analytical approach, was chosen for evaluation due to its combined design and analysis capabilities. The inlet design produced by IPSSO was then analyzed using the NASTRAN finite element program. The finite element analysis was performed to help identify the limitations of the analytically based code as well as to evaluate NASTRAN for this application. Comparison between the IPSSO inlet weight and that of a similar inlet developed by the Boeing Commercial Airplane Group was also made. Program evaluation concluded that the combined use of IPSSO to create an initial design and NASTRAN to perform a numerical analysis would provide the capability to evaluate a limited number of inlet design The development of a new tool for the minimum weight design and analysis of inlet structures would be required for greater flexibility in evaluating inlet conceptual designs. Nadell, Shari-Beth Glenn Research Center RTOP 505-69-50...

Book NASA Technical Paper

Download or read book NASA Technical Paper written by and published by . This book was released on 1985 with total page 80 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 The Aerothermodynamics of Aircraft Gas Turbine Engines

Download or read book The Aerothermodynamics of Aircraft Gas Turbine Engines written by and published by . This book was released on 1978 with total page 770 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 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 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book The Aeronautical Journal

Download or read book The Aeronautical Journal written by and published by . This book was released on 1975 with total page 660 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book NASA Contractor Report

Download or read book NASA Contractor Report written by and published by . This book was released on 1976 with total page 556 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Technical Abstract Bulletin

Download or read book Technical Abstract Bulletin written by and published by . This book was released on with total page 812 pages. Available in PDF, EPUB and Kindle. Book excerpt: