Advances in Aeronautical Sciences 1959
DOI: 10.1016/b978-1-4831-9833-0.50006-2
|View full text |Cite
|
Sign up to set email alerts
|

Fundamental Design Problems of Aircraft With Boundary Layer Control for Maintaining Laminar Flow

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
2
1

Citation Types

0
1
0

Year Published

1961
1961
2024
2024

Publication Types

Select...
4
1
1

Relationship

0
6

Authors

Journals

citations
Cited by 6 publications
(7 citation statements)
references
References 4 publications
0
1
0
Order By: Relevance
“…[63~65] 、湍流边界层理论 [63] 、三维边界层 理论 [34,66,67] 、流动稳定性理论 [68,69] 、转捩理论 [35,70] 、 边界层控制理论 [70,71] 和可压缩边界层理论 [62,72,73] .…”
Section: 得益于电子计算机技术的进步 以直接数值模拟unclassified
“…[63~65] 、湍流边界层理论 [63] 、三维边界层 理论 [34,66,67] 、流动稳定性理论 [68,69] 、转捩理论 [35,70] 、 边界层控制理论 [70,71] 和可压缩边界层理论 [62,72,73] .…”
Section: 得益于电子计算机技术的进步 以直接数值模拟unclassified
“…Additionally, insect density decreases rapidly from ground level to an altitude of 150 m [155]. Insect-free environments are more prevalent in very low temperatures and low humidity [156]. The conditions conducive to insect contamination are illustrated in Figure 15.…”
Section: Insectsmentioning
confidence: 99%
“…Additionally, insect density decreases rapidly from ground level to an altitude of 150 m [158]. Insect-free environments are more prevalent in very low temperatures and low humidity [159]. The conditions conducive to insect contamination are illustrated in Error!…”
Section: Insectsmentioning
confidence: 99%