High Reynolds number tests of a Douglas DLBA 032 airfoil in the Langley 0.3-meter transonic cryogenic tunnel
By: Charles B. Johnson ... [et al.].
Contributors: Johnson, Charles B.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Series: NASA technical memorandum -- 87663.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch
Published: 1988
Place of publication: [Washington, D.C.]
Language: eng
Format: Microform
Subjects: Aerodynamics.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1988. 2 microfiches.