Vapor-screen flow-visualization experiments in the NASA Langley 0.3-m transonic cryogenic tunnel
By: Gregory Vincent Selby.
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.; Langley Research Center.
Series: NASA contractor report -- 3984.; NASA contractor report -- NASA CR-3984.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch
Published: 1986
Place of publication: [Washington, D.C.]
Language: eng
Format: Microform
Subjects: Delta wing airplanes.; Low temperature engineering.; Transonic wind tunnels.; Vortex-motion.; Wind tunnels -- Flow visualization.; Condensation.; Cryogenic wind tunnels.; Delta wings.; Flow visualization.; Vortices.; Wind tunnel models.
Notes: "Prepared for Langley Research Center under grant NGT 48-003-029."

Includes bibliographical references.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration,] 1986. 1 microfiche.