Research Catalog

Experiments on two opposed lateral jets injected into swirling crossflow

Title
Experiments on two opposed lateral jets injected into swirling crossflow / by C.B. McMurry and D.G. Lilley.
Author
McMurry, Carl Burton, 1961-
Publication
Cleveland, Ohio : Lewis Research Center, [National Aeronautics and Space Administration] ; Stillwater, Okla. : Oklahoma State University, School of Mechanical and Aerospace Engineering, [1986]

Details

Additional Authors
  • Lilley, D. G.
  • Oklahoma State University. School of Mechanical and Aerospace Engineering, issuing body.
  • United States. National Aeronautics and Space Administration, sponsoring body.
  • Lewis Research Center.
Description
1 microfiche (iii, 112 pages) : negative, illustrations; 11 x 15 cm.
Summary
"Experiments have been conducted to obtain the time-mean and turbulent quantities of opposed lateral jets in a low speed, nonreacting flowfield. A jet-to-crossflow velocity ratio of R = v sub J u sub 0 = 4 was used throughout the experiments, with swirl vane angles of d = 0 (swirler removed), 45 and 70 deg used with the crossflow. Flow visualization techniques used were neutrally-buoyant helium-filled soap bubbles and multispark photography in order to obtain the gross flowfield characteristics. Measurements of time-mean and turbulent quantities were obtained utilizing a six-orientation single hot-wire technique. For the nonswirling case, the jets were found not to penetrate past the test-section centerline, in contrast to the single lateral jet with the same jet-to-crossflow velocity ratio. In the swirling cases, the crossflow remains in a narrow region near the wall of the test section. The opposed jets are swept from their vertical courses into spiral trajectories close to the confining walls. Extensive results are presented in r-x plane plots."--NTIS abstract.
Series Statement
NASA contractor report ; 175041
Uniform Title
NASA contractor report ; NASA CR-175041.
Subject
  • Combustion chambers > Aerodynamics
  • Cross-flow (Aerodynamics)
  • Jets > Fluid dynamics
  • Turbulence
  • Flow distribution
  • Swirling
  • Turbulent jets
  • Turbulent mixing
  • Combustion chambers; Flow distribution; Swirling; Turbulent jets; Turbulent mixing; Hot-wire anemometers; Lateral control
Note
  • "January 1986."
  • "This report was a dissertation submitted by C.B. McMurry to the faculty of the Graduate College of Oklahoma State University in partial fulfullment of the requirements for the degree Master of Science in December 1985."
  • "Performing organization: Oklahoma State University, School of Mechanical and Aerospace Engineering ; sponsoring agency: National Aeronautics and Space Administration."
Bibliography (note)
  • Includes bibliographical references (pages 23-24).
Funding (note)
  • Prepared for Lewis Research Center under grant
Call Number
GPO Microfiche NAS 1.26:175041
OCLC
marcive236111349
Author
McMurry, Carl Burton, 1961- author.
Title
Experiments on two opposed lateral jets injected into swirling crossflow / by C.B. McMurry and D.G. Lilley.
Publisher
Cleveland, Ohio : Lewis Research Center, [National Aeronautics and Space Administration] ; Stillwater, Okla. : Oklahoma State University, School of Mechanical and Aerospace Engineering, [1986]
Type of Content
text
Type of Medium
microform
Type of Carrier
microfiche
Series
NASA contractor report ; 175041
NASA contractor report ; NASA CR-175041.
Bibliography
Includes bibliographical references (pages 23-24).
Funding
Prepared for Lewis Research Center under grant NAG 3-549 533-04-1A
Indexed Term
Combustion chambers; Flow distribution; Swirling; Turbulent jets; Turbulent mixing; Hot-wire anemometers; Lateral control
Added Author
Lilley, D. G., author.
Oklahoma State University. School of Mechanical and Aerospace Engineering, issuing body.
United States. National Aeronautics and Space Administration, sponsoring body.
Lewis Research Center.
Other Form:
Print version: McMurry, Carl Burton, 1961- Experiments on two opposed lateral jets injected into swirling crossflow. (OCoLC)842846435
Gpo Item No.
0830-H-14 (MF)
Sudoc No.
NAS 1.26:175041
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