Design And Analysis Tool For External Compression Supersonic Inlets
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Author |
: National Aeronautics and Space Administration (NASA) |
Publisher |
: Createspace Independent Publishing Platform |
Total Pages |
: 26 |
Release |
: 2018-05-22 |
ISBN-10 |
: 1719390401 |
ISBN-13 |
: 9781719390408 |
Rating |
: 4/5 (01 Downloads) |
Synopsis Design and Analysis Tool for External-Compression Supersonic Inlets by : National Aeronautics and Space Administration (NASA)
A computational tool named SUPIN has been developed to design and analyze external-compression supersonic inlets for aircraft at cruise speeds from Mach 1.6 to 2.0. The inlet types available include the axisymmetric outward-turning, two-dimensional single-duct, two-dimensional bifurcated-duct, and streamline-traced Busemann inlets. The aerodynamic performance is characterized by the flow rates, total pressure recovery, and drag. The inlet flowfield is divided into parts to provide a framework for the geometry and aerodynamic modeling and the parts are defined in terms of geometric factors. The low-fidelity aerodynamic analysis and design methods are based on analytic, empirical, and numerical methods which provide for quick analysis. SUPIN provides inlet geometry in the form of coordinates and surface grids useable by grid generation methods for higher-fidelity computational fluid dynamics (CFD) analysis. SUPIN is demonstrated through a series of design studies and CFD analyses were performed to verify some of the analysis results. Slater, John W. Glenn Research Center COMPUTATIONAL FLUID DYNAMICS; SUPERSONIC INLETS; FLOW DISTRIBUTION; AERODYNAMIC CHARACTERISTICS; DRAG; FLOW VELOCITY; SUPERSONIC SPEED; DUCTS; PRESSURE RECOVERY; DESIGN ANALYSIS
Author |
: John W. Slater |
Publisher |
: |
Total Pages |
: 23 |
Release |
: 2012 |
ISBN-10 |
: OCLC:821666277 |
ISBN-13 |
: |
Rating |
: 4/5 (77 Downloads) |
Synopsis Design and analysis tool for external-compression supersonic inlets by : John W. Slater
Author |
: John W. Slater |
Publisher |
: BiblioGov |
Total Pages |
: 32 |
Release |
: 2013-07 |
ISBN-10 |
: 1289151458 |
ISBN-13 |
: 9781289151454 |
Rating |
: 4/5 (58 Downloads) |
Synopsis Design and Analysis Tool for External-Compression Supersonic Inlets by : John W. Slater
A computational tool named SUPIN has been developed to design and analyze external-compression supersonic inlets for aircraft at cruise speeds from Mach 1.6 to 2.0. The inlet types available include the axisymmetric outward-turning, two-dimensional single-duct, two-dimensional bifurcated-duct, and streamline-traced Busemann inlets. The aerodynamic performance is characterized by the flow rates, total pressure recovery, and drag. The inlet flowfield is divided into parts to provide a framework for the geometry and aerodynamic modeling and the parts are defined in terms of geometric factors. The low-fidelity aerodynamic analysis and design methods are based on analytic, empirical, and numerical methods which provide for quick analysis. SUPIN provides inlet geometry in the form of coordinates and surface grids useable by grid generation methods for higher-fidelity computational fluid dynamics (CFD) analysis. SUPIN is demonstrated through a series of design studies and CFD analyses were performed to verify some of the analysis results.
Author |
: Thomas J. Benson |
Publisher |
: |
Total Pages |
: 18 |
Release |
: 1994 |
ISBN-10 |
: NASA:31769000607278 |
ISBN-13 |
: |
Rating |
: 4/5 (78 Downloads) |
Synopsis An Interactive, Design and Educational Tool for Supersonic External-compression Inlets by : Thomas J. Benson
Author |
: John W. Slater |
Publisher |
: BiblioGov |
Total Pages |
: 26 |
Release |
: 2013-06 |
ISBN-10 |
: 1289062382 |
ISBN-13 |
: 9781289062385 |
Rating |
: 4/5 (82 Downloads) |
Synopsis External-Compression Supersonic Inlet Design Code by : John W. Slater
The NASA Technical Reports Servcr (NTRS) houses half a million publications that are a valuable means of information to researchers, teachers, students, and the general public. These documents are all aerospace related with much scientific and technical information created or funded by NASA. Some types of documents include conference papers, research reports, meeting papers, journal articles and more. This is one of those documents.
Author |
: Larry W. Pennel |
Publisher |
: |
Total Pages |
: 72 |
Release |
: 1973 |
ISBN-10 |
: OCLC:881958 |
ISBN-13 |
: |
Rating |
: 4/5 (58 Downloads) |
Synopsis Preliminary Design Analysis of an External Compression Inlet for the B-1 Aircraft by : Larry W. Pennel
Author |
: National Aeronautics and Space Administration (NASA) |
Publisher |
: Createspace Independent Publishing Platform |
Total Pages |
: 32 |
Release |
: 2018-06-24 |
ISBN-10 |
: 1721804285 |
ISBN-13 |
: 9781721804283 |
Rating |
: 4/5 (85 Downloads) |
Synopsis Planar Inlet Design and Analysis Process (Pindap) by : National Aeronautics and Space Administration (NASA)
The Planar Inlet Design and Analysis Process (PINDAP) is a collection of software tools that allow the efficient aerodynamic design and analysis of planar (two-dimensional and axisymmetric) inlets. The aerodynamic analysis is performed using the Wind-US computational fluid dynamics (CFD) program. A major element in PINDAP is a Fortran 90 code named PINDAP that can establish the parametric design of the inlet and efficiently model the geometry and generate the grid for CFD analysis with design changes to those parameters. The use of PINDAP is demonstrated for subsonic, supersonic, and hypersonic inlets. Slater, John W. and Gruber, Christopher R. Glenn Research Center NASA/TM-2005-213866, E-15236, AIAA Paper 2005-4203
Author |
: |
Publisher |
: |
Total Pages |
: 542 |
Release |
: 1995 |
ISBN-10 |
: MINN:31951P004956173 |
ISBN-13 |
: |
Rating |
: 4/5 (73 Downloads) |
Synopsis Scientific and Technical Aerospace Reports by :
Author |
: Ambrish Maurya |
Publisher |
: Springer Nature |
Total Pages |
: 880 |
Release |
: 2023-06-07 |
ISBN-10 |
: 9789811977091 |
ISBN-13 |
: 9811977097 |
Rating |
: 4/5 (91 Downloads) |
Synopsis Recent Trends in Mechanical Engineering by : Ambrish Maurya
This book contains the select papers presented at the International Conference on Progressive Research in Industrial & Mechanical Engineering (PRIME 2021), held at the National Institute of Technology (NIT) Patna, India. The book discusses various aspects related and relevant to core areas of mechanical engineering including engineering design, production engineering, industrial engineering, automobile engineering, thermal and fluids engineering, mechatronics, control and robotics and other inter-disciplinary emerging topics for potential use in a spectrum of applications. The book will be a valuable reference for students, researchers and professionals interested in mechanical engineering and allied fields.
Author |
: J. E. Hawkins |
Publisher |
: |
Total Pages |
: 114 |
Release |
: 1976 |
ISBN-10 |
: NASA:31769000498504 |
ISBN-13 |
: |
Rating |
: 4/5 (04 Downloads) |
Synopsis Inlet Spillage Drag Tests and Numerical Flow-field Analysis at Subsonic and Transonic Speeds of a 1/8-scale, Two-dimensional, External-compression, Variable-geometry, Supersonic Inlet Configuration by : J. E. Hawkins