Aircraft Systems, Design and Technology Meeting 1986
DOI: 10.2514/6.1986-2752
|View full text |Cite
|
Sign up to set email alerts
|

Wind tunnel tests in student design projects - A useful tool

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1

Citation Types

0
1
0

Year Published

1996
1996
1997
1997

Publication Types

Select...
2

Relationship

0
2

Authors

Journals

citations
Cited by 2 publications
(1 citation statement)
references
References 1 publication
0
1
0
Order By: Relevance
“…Thus, for example, the airfoil sizing/geometry selection procedure of Raymer [4] could not be used. On the other hand, team members did run a computational aerodynamics program, perform wind-tunnel tests (with all the academic benefits of such testing [9]), look at stall characteristics, calculate lift coefficients, and do a myriad of other technical activities that have enhanced their understanding of aerodynamics. Similarly, the group involved in the aircraft structural design learned important lessons about structural 56 Sheldon I.…”
Section: Merits and Limitations Of Model Airplane Competitions As A Fmentioning
confidence: 99%
“…Thus, for example, the airfoil sizing/geometry selection procedure of Raymer [4] could not be used. On the other hand, team members did run a computational aerodynamics program, perform wind-tunnel tests (with all the academic benefits of such testing [9]), look at stall characteristics, calculate lift coefficients, and do a myriad of other technical activities that have enhanced their understanding of aerodynamics. Similarly, the group involved in the aircraft structural design learned important lessons about structural 56 Sheldon I.…”
Section: Merits and Limitations Of Model Airplane Competitions As A Fmentioning
confidence: 99%