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Book Pressure Distributions for a Rectangular Supersonic Inlet at Subsonic Speeds

Download or read book Pressure Distributions for a Rectangular Supersonic Inlet at Subsonic Speeds written by Dennis E. Fuller and published by . This book was released on 1976 with total page 484 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Pressure Distributions for a Rectangular Supersonic Inlet at Subsonic Speeds

Download or read book Pressure Distributions for a Rectangular Supersonic Inlet at Subsonic Speeds written by Dennis E. Fuller and published by . This book was released on 1976 with total page 844 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Effect of Yaw and Angle of Attack on Pressure Recovery and Mass flow Characteristics of a Rectangular Supersonic Scoop Inlet at a Mach Number of 2 71

Download or read book Effect of Yaw and Angle of Attack on Pressure Recovery and Mass flow Characteristics of a Rectangular Supersonic Scoop Inlet at a Mach Number of 2 71 written by Raymond J. Comenzo and published by . This book was released on 1954 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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 Scientific and Technical Aerospace Reports

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1965 with total page 1068 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book A Full Navier Stokes Analysis of Subsonic Diffuser of a Bifurcated 70 30 Supersonic Inlet for High Speed Civil Transport Application

Download or read book A Full Navier Stokes Analysis of Subsonic Diffuser of a Bifurcated 70 30 Supersonic Inlet for High Speed Civil Transport Application written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-08-09 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: A full Navier-Stokes analysis was performed to evaluate the performance of the subsonic diffuser of a NASA Lewis Research Center 70/30 mixed-compression bifurcated supersonic inlet for high speed civil transport application. The PARC3D code was used in the present study. The computations were also performed when approximately 2.5 percent of the engine mass flow was allowed to bypass through the engine bypass doors. The computational results were compared with the available experimental data which consisted of detailed Mach number and total pressure distribution along the entire length of the subsonic diffuser. The total pressure recovery, flow distortion, and crossflow velocity at the engine face were also calculated. The computed surface ramp and cowl pressure distributions were compared with experiments. Overall, the computational results compared well with experimental data. The present CFD analysis demonstrated that the bypass flow improves the total pressure recovery and lessens flow distortions at the engine face. Kapoor, Kamlesh and Anderson, Bernhard H. and Shaw, Robert J. Glenn Research Center NASA-TM-106637, E-8939, NAS 1.15:106637 RTOP 537-02-23...

Book STAR

    Book Details:
  • Author :
  • Publisher :
  • Release : 1973
  • ISBN :
  • Pages : 904 pages

Download or read book STAR written by and published by . This book was released on 1973 with total page 904 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Monthly Catalog of United States Government Publications  Cumulative Index

Download or read book Monthly Catalog of United States Government Publications Cumulative Index written by United States. Superintendent of Documents and published by . This book was released on 1976 with total page 1408 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Applied Mechanics Reviews

Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1952 with total page 626 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Research and Technology Objectives and Plans Summary

Download or read book Research and Technology Objectives and Plans Summary written by and published by . This book was released on with total page 244 pages. Available in PDF, EPUB and Kindle. Book excerpt: "A compilation of the summary portions of each of the RTOPs used for management review and control of research currently in progress throughout NASA"--P. i.

Book Monthly Catalog of United States Government Publications

Download or read book Monthly Catalog of United States Government Publications written by United States. Superintendent of Documents and published by . This book was released on 1960 with total page 1812 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book An Implicit Method for the Calculation of Inlet Flow Fields

Download or read book An Implicit Method for the Calculation of Inlet Flow Fields written by Sedat Biringen and published by . This book was released on 1981 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt: Inlet flow fields are calculated by an implicit, time marching procedure to solve the thin layer Navier-Stokes equations formulated in body fitted coordinates. Because the method can be used for a flow field with both subsonic and supersonic regions, it is applicable to subcritical as well as supercritical inlet operation. Results are presented and discussed for an inlet of current design practice. Results include inviscid calculations performed for supercritical inlet operation with uniform and nonuniform inflow boundary conditions as well as for subcritical inlet operation with uniform inflow boundary conditions. Results for viscous calculations performed for supercritical inlet operation with uniform inflow boundary conditions are also discussed.

Book A Numerical Integration Method for Calculation the Pressure Distribution at Supersonic Speeds for Wings with Subsonic Leading Edge at Symmetrical Flow Conditions

Download or read book A Numerical Integration Method for Calculation the Pressure Distribution at Supersonic Speeds for Wings with Subsonic Leading Edge at Symmetrical Flow Conditions written by V. V. Linnaluoto and published by . This book was released on 1952 with total page 19 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book An Introductory Guide to EC Competition Law and Practice

Download or read book An Introductory Guide to EC Competition Law and Practice written by Valentine Korah and published by . This book was released on 1994 with total page 2354 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Bypass duct Design for Use with Supersonic Inlets

Download or read book Bypass duct Design for Use with Supersonic Inlets written by Charles C. Wood and published by . This book was released on 1956 with total page 14 pages. Available in PDF, EPUB and Kindle. Book excerpt: