Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wingSheryll Goecke Powers · First published 1997Open the Tome
Women in flight research at NASA Dryden Flight Research Center from 1946 to 1995Sheryll Goecke Powers · First published 1997Open the Tome
Flight and wind-tunnel measurements showing base drag reduction provided by a trailing disk for high Reynolds number turbulent flow for subsonic and transonic Mach numbersSheryll Goecke Powers · First published 1986 · Latest edition 1988Open the Tome
Flight tests of external modifications used to reduce blunt base dragSheryll Goecke Powers · First published 1988Open the Tome
Influence of base modifications on in-flight base drag in the presence of jet exhaust for Mach numbers from 0.7 to 1.5Sheryll Goecke Powers · First published 1988Open the Tome
Flight-measured pressure characteristics of aft-facing steps in high Reynolds number flow at Mach numbers of 2.20, 2.50, and 2.80 and comparison with other dataSheryll Goecke Powers · First published 1978Open the Tome
Flight-measured pressure characteristics of aft-facing steps in high Reyonlds number flow at Mach numbers of 2.20, 2.50, and 2.80 and comparison with other dataSheryll Goecke Powers · First published 1978Open the Tome
