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Effect of shortening transition liner to decrease overall length of a ram induction combustor / by Donald F. Schultz, Porter J. Perkins, and Jerrold D. Wear.

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U.S. Government Documents
Format:
Book
Government document
Author/Creator:
Schultz, Donald F., author.
Perkins, Porter J., author.
Wear, Jerrold D., author.
Contributor:
United States. National Aeronautics and Space Administration, issuing body.
Lewis Research Center
Series:
NASA technical note ; D-7021.
NASA/TN ; D-7021
Language:
English
Subjects (All):
Airplanes--Turbojet engines--Combustion.
Airplanes.
Smoke.
Combustion--Research.
Combustion.
smoking (preserving).
smoking (activity).
smoke (material).
Combustion chambers--Testing.
Physical Description:
1 online resource (18 pages) : illustrations
Place of Publication:
Washington, D.C. : National Aeronautics and Space Administration, December 1970.
Notes:
"December 1970."
Includes bibliographical references (pages 17-18).
Online resource, PDF version; title from title page (NASA, viewed on June 23, 2021).
Other Format:
Print version: Schultz, Donald F. Effect of shortening transition liner to decrease overall length of a ram induction combustor.
OCLC:
761140144

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