To develop configurations suitable for long range hypersonic gliders, geometric study is made of some of effects of dihedral on heat transfer to swept delta wings; other conditions indicated.
Influence of large positive dihedral on heat transfer to leading edges of highly swept wings at very high mach numbers
NASA -- Memo
1959
18 pages
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Critical mach numbers for swept-back wings
Engineering Index Backfile | 1950
|Transition on swept leading edges at Mach 3.5
NTRS | 1987
|Transition on swept leading edges at Mach 3.5
AIAA | 1987
|