Wind-tunnel/flight correlation study of aerodynamic characteristics of a large flexible supersonic cruise airplane (XB-70-1).
Contributors: Daugherty, James C.; Peterson, John B.; Arnaiz, Henry H.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.; Ames Research Center.; Langley Research Center.
Series: NASA technical paper -- 1514, 1515, 1516.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1979
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Subjects: Aerodynamics, Supersonic.; Wind tunnels -- Experiments.
Notes: "Ames Research Center"--Vol. 1.

"Langley Research Center"--Vol. 2.

"dryden Flight Research Center"--Vol. 3.

"NASA. Scientific and Technical Information Branch"--Vol. 1.

"NASA. Scientific and Technical Information Office"--Vols. 2 & 3.
Table of contents: value: 1. Wind-tunnel tests of a 0.03-scale model at Mach numbers from 0.6 to 2.53 / James C. Daugherty; value: 2. Extrapolation of wind-tunnel data to full-scale conditions / John B. Peterson [et al.].; value: 3. A comparision between characteristics predicted from wind-tunnel measurements and those measured in flight / Arnaiz, Henry H.