Tests at a Mach Number of 2.0 on a Rectangular, Twin-duct Air Intake with Variable Geometry, Situated in a Flow Field of a Slender Wing

preview-18
  • Tests at a Mach Number of 2.0 on a Rectangular, Twin-duct Air Intake with Variable Geometry, Situated in a Flow Field of a Slender Wing Book Detail

  • Author : M. D. Dobson
  • Release Date : 1968
  • Publisher :
  • Genre :
  • Pages : 37
  • ISBN 13 :
  • File Size : 4,4 MB

Tests at a Mach Number of 2.0 on a Rectangular, Twin-duct Air Intake with Variable Geometry, Situated in a Flow Field of a Slender Wing by M. D. Dobson PDF Summary

Book Description:

Disclaimer: www.yourbookbest.com does not own Tests at a Mach Number of 2.0 on a Rectangular, Twin-duct Air Intake with Variable Geometry, Situated in a Flow Field of a Slender Wing books pdf, neither created or scanned. We just provide the link that is already available on the internet, public domain and in Google Drive. If any way it violates the law or has any issues, then kindly mail us via contact us page to request the removal of the link.

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports

File Size : 69,69 MB
Total View : 2732 Views
DOWNLOAD

Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the N

Aeronautical Engineering

Aeronautical Engineering

File Size : 79,79 MB
Total View : 2777 Views
DOWNLOAD

A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system