A feasibility study of using Langley 0.3-m Transonic Cryogenic Tunnel sidewall boundary-layer removable system for heavy gas testing
By: A.V. Murthy, S. Balakrishna, and W. Allen Kilgore.
Contributors: Balakrishna, S.; Kilgore, W. Allen.; Langley Research Center.
Series: NASA contractor report -- 191438.; NASA contractor report -- NASA CR-191438.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1993
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Transonic wind tunnels.; Boundary layer.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 93-1026-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1993] 1 microfiche.