Sonic Boom Testing of Artificially Blunted Leading Edge (ABLE) Concepts in the NASA Ames Aeroballistic Range
38th, Aerospace sciences meeting ; 2000 ; Reno, NV
01.01.2000
ALL
Paper nos AIAA-2000-0001 to AIAA-2000-1076 with gaps
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
NTRS | 2009
|Optimal Artificially Blunted Leading-Edge Airfoils for Enhanced Aerothermodynamic Performance
Online Contents | 1999
|