High Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-meter transonic cryogenic tunnel
By: William G. Johnson ... [et al.]
Contributors: Johnson, William G. 1944-; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
Series: NASA technical memorandum -- 81922
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch
Published: 1982
Place of publication: [Washington, D.C.?]
Language: eng
Format: Microform
Subjects: Aerofoils; Reynolds number; Aerodynamics, Transonic; Transonic wind tunnels
Notes: "N84-27684"--Microfiche header

Includes bibliographical references

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration, 1984]. 2 microfiches ; 11 x 15 cm