Research Catalog

  • Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controlled inlet-stability bypass system when subjected to internal and external airflow transients / Bobby W. Sanders.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office, January 1980.
    • 1980-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo52217

No results found from Digital Research Books Beta

Digital books for research from multiple sources world wide- all free to read, download, and keep. No Library Card is Required. Read more about the project.

digital-research-book
Explore Digital Research Books Beta