Application of shock tubes to transonic airfoil testing at high Reynolds number
By: William J. Cook ... [et al.], Iowa State University
Contributors: Cook, William John, 1929-; Iowa State University
Series: NASA technical paper ; 1268
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Office; for sale by the National Technical Information Service
Published: 1978
Place of publication: [Washington]; Springfield, Va
Language: eng
Number of pages: 63
Subjects: Shock tubes; Aerofoils
Notes: Nov. 1978

Includes bibliographical references