Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing

Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing [microform] / Sheryll Goecke Powers and Lannie D. Webb.

Show other versions (1)
Saved in:
Bibliographic Details
Main Author: Powers, Sheryll Goecke
Corporate Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Program
Other Authors: Webb, Lannie D.
Format: Government Document Microfilm Book
Language:English
Published: [Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [National Technical Information Service, distributor], 1997.
Series:NASA technical memorandum ; 4789.
Subjects:
Flight control.
Mach number.
Reynolds number.
Pressure > Measurement.
Flight tests.
Boundary layers.
Swept wings.
Pressure distribution.
Angle of attack.
Supercritical wings.
Pressure measurement.

Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number: NAS 1.15:4789
NAS 1.15:4789 Restricted Place a Hold

Similar Items