DBD plasma actuators for flow control in air vehicles and jet engines : simulation of flight conditions in test chambers by density matching

Title
  1. DBD plasma actuators for flow control in air vehicles and jet engines : simulation of flight conditions in test chambers by density matching / David E. Ashpis, Douglas R. Thurman.
Published by
  1. Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2011.
Author
  1. Ashpis, D. E. (David E.)

Details

Additional authors
  1. Thurman, Douglas R.
  2. NASA Glenn Research Center, issuing body.
  3. United States. National Aeronautics and Space Administration, sponsoring body.
  4. U.S. Army Research Laboratory, sponsoring body.
Description
  1. 1 online resource (31 pages) : color illustrations.
Series statement
  1. NASA/TM ; 2011-217006/REV1
Uniform title
  1. DBD plasma actuators for flow control in air vehicles and jet engines (Revised July 2011)
  2. NASA technical memorandum ; 2011-217006/REV 1.
Alternative title
  1. DBD plasma actuators for flow control in air vehicles and jet engines (Revised July 2011)
  2. Dielectric Barrier Discharge plasma actuators for flow control in air vehicles and jet engines
Subject
  1. Jet engines
  2. Actuators
  3. Active control
  4. Dielectrics
  5. Gas density
  6. Turbines
  7. Pressure distribution
  8. Plasma jets
  9. Magnetohydrodynamic flow
Call number
  1. GPO Internet NAS 1.15:2011-217006/REV.1
Note
  1. Title from title screen (viewed on Feb. 4, 2014).
  2. "July 2011."
  3. "Prepared for the 42nd Plasmadynamics and Lasers Conference sponsored by the American Institute of Aeronautics and Astronautics Honolulu, Hawaii, June 27-30, 2011."
  4. "AIAA-2011-3730."
  5. "This printing replaces NASA/TM--2011-217006, March 2011"--Report documentation page.
Bibliography (note)
  1. Includes bibliographical references (pages 7-8).
Funding (note)
  1. Sponsored by National Aeronautics and Space Administration and U.S. Army Research Laboratory
Author
  1. Ashpis, D. E. (David E.), author.
Title
  1. DBD plasma actuators for flow control in air vehicles and jet engines : simulation of flight conditions in test chambers by density matching / David E. Ashpis, Douglas R. Thurman.
Publisher
  1. Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2011.
Edition
  1. [Revised].
Type of content
  1. text
Type of medium
  1. computer
Type of carrier
  1. online resource
Series
  1. NASA/TM ; 2011-217006/REV1
  2. NASA technical memorandum ; 2011-217006/REV 1.
Bibliography
  1. Includes bibliographical references (pages 7-8).
Funding
  1. Sponsored by National Aeronautics and Space Administration and U.S. Army Research Laboratory WBS 561581.02.08.03.21.13.02
  2. E-17602-1
Connect to:
  1. https://purl.fdlp.gov/GPO/gpo45706
Added author
  1. Thurman, Douglas R., author.
  2. NASA Glenn Research Center, issuing body.
  3. United States. National Aeronautics and Space Administration, sponsoring body.
  4. U.S. Army Research Laboratory, sponsoring body.
Gpo item no.
  1. 0830-D (online)
Sudoc no.
  1. NAS 1.15:2011-217006/REV.1
View in legacy catalog