EBookClubs

Read Books & Download eBooks Full Online

EBookClubs

Read Books & Download eBooks Full Online

Book Real helium Hypersonic Flow Parameters for Pressures to 3600 Atmospheres and Temperatures to 15 000   K

Download or read book Real helium Hypersonic Flow Parameters for Pressures to 3600 Atmospheres and Temperatures to 15 000 K written by Charles George Miller and published by . This book was released on 1968 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book NASA Technical Note

    Book Details:
  • Author :
  • Publisher :
  • Release : 1968
  • ISBN :
  • Pages : 452 pages

Download or read book NASA Technical Note written by and published by . This book was released on 1968 with total page 452 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 1969 with total page 362 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book A Selected Listing of NASA Scientific and Technical Reports

Download or read book A Selected Listing of NASA Scientific and Technical Reports written by United States. National Aeronautics and Space Administration. Scientific and Technical Information Division and published by . This book was released on 1970 with total page 962 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book NASA Scientific and Technical Reports and Publications for 1969   A Selected Listing

Download or read book NASA Scientific and Technical Reports and Publications for 1969 A Selected Listing written by United States. National Aeronautics and Space Administration. Scientific and Technical Information Division and published by . This book was released on 1970 with total page 956 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book NASA Scientific and Technical Reports

Download or read book NASA Scientific and Technical Reports written by United States. National Aeronautics and Space Administration Scientific and Technical Information Division and published by . This book was released on 1970 with total page 966 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Real Gas Flow Parameters for NASA Langley 22 inch Mach 20 Helium Tunnel

Download or read book Real Gas Flow Parameters for NASA Langley 22 inch Mach 20 Helium Tunnel written by Brian R. Hollis and published by . This book was released on 1992 with total page 74 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Bulletin of Thermodynamics and Thermochemistry

Download or read book Bulletin of Thermodynamics and Thermochemistry written by and published by . This book was released on 1974 with total page 696 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 1969 with total page 1090 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 1979 with total page 1504 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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 1966 with total page 1464 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book A Performance Study of a Piston Compression Shock Tunnel

Download or read book A Performance Study of a Piston Compression Shock Tunnel written by G. P. Rouel and published by . This book was released on 1973 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt: A theoretical study of a high performance piston compression tailored mode reflected shock tunnel, designed to achieve re-entry flow simulation, has been carried out. The designed tunnel supply conditions were pressures varying from 2000 to 5000 atm at temperatures from 6000 to 12,000K. The pressures and temperatures involved in the study were high enough that imperfections in the equation of state covering both dense gas effects and internal energy modes were required to be assumed. Similar running times as in conventional shock tunnels have been shown to be achieved at the design performance with relatively lowly stressed tube extensions. Helium is shown to be a more efficient driver gas than hydrogen in piston compression operation in terms of both performance and running time. (Modified author abstract).

Book Real gas Correction Factors for Hypersonic Flow Parameters in Helium

Download or read book Real gas Correction Factors for Hypersonic Flow Parameters in Helium written by Wayne Douglas Erickson and published by . This book was released on 1960 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt: The real-gas hypersonic flow parameters for helium have been calculated for stagnation temperatures from 0 F to 600 F and stagnation pressures up to 6,000 pounds per square inch absolute. The results of these calculations are presented in the form of simple correction factors which must be applied to the tabulated ideal-gas parameters. It has been shown that the deviations from the ideal-gas law which exist at high pressures may cause a corresponding significant error in the hypersonic flow parameters when calculated as an ideal gas. For example the ratio of the free-stream static to stagnation pressure as calculated from the thermodynamic properties of helium for a stagnation temperature of 80 F and pressure of 4,000 pounds per square inch absolute was found to be approximately 13 percent greater than that determined from the ideal-gas tabulation with a specific heat ratio of 5/3.