Variable Sweep Transition Flight Experiment (VSTFE)
Subtitle: Parametric Pressure Distribution Boundary Layer Stability Study and wing glove design task
By: Rodger A. Rozendaal.
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Series: NASA contractor report -- 3992.; NASA contractor report -- NASA CR-3992.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch
Published: 1988
Place of publication: [Washington, DC]
Language: eng
Format: Microform
Subjects: Fluid dynamics.
Notes: Distributed to depository libraries in microfiche.

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