Wind-tunnel/flight correlation study of aerodynamic characteristics of a large flexible supersonic cruise airplane (XB-70-1)
By: Henry H. Arnaiz, Dryden Flight Research Center, John B. Peterson, Jr., Langley Research Center, James C. Daugherty, Ames Research Center
Contributors: Peterson, John B., joint author; Daugherty, James C., joint author; Hugh L. Dryden Flight Research Center; Langley Research Center; Ames Research Center; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office
Series: NASA technical paper ; 1516
Publisher: Nationa1 Aeronautics and Space Administration, Scientific and Technica1 Information Office; for sa1e by the Nationa1 Technica1 Information Service]
Published: 1980
Place of publication: [Washington]
Language: eng
Subjects: Aerodynamics, Supersonic; Wind tunnel models
Notes: March 1980
Table of contents: III. A comparison between characteristics predicted from wind-tunnel measurements and those measured in flight; 1. Wind-tunnel tests of a 0.03-scale model at Mach numbers from 0.6 to 2.53 / James C. Daugherty; 2. Extrapolation of wind-tunnel data to full-scale conditions / John B. Peterson [et al.]