Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel
By: Glen P. Doggett and Ndaona Chokani.
Contributors: Chokani, Ndaona.; Langley Research Center.
Series: NASA contractor report -- 201617; NASA contractor report -- NASA CR-201617.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1996
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Angle of attack.; Aerodynamic noise.; Zero angle of attack.; Boundary layer stability.; Hypersonic speed.; Navier-Stokes equation.; Hypersonics.; Aerodynamic stability.; Hypersonic boundary layer.
Other titles: Hypersonic boundadry layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 98-0277-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 2 microfiches.