Span load distributions resulting from constant vertical acceleration for thin sweptback tapered wings with streamwise tips. : Supersonic leading and trailing edges / Isabella J. Cole and Kenneth Margolis.
On the basis of the linearized supersonic-flow theory, equations for the span load distribution resulting from constant vertical acceleration (that is, linear variation of angle of attack with time) are derived for a series of thin sweptback tapered wings with streamwise tips. The analysis is valid...
Saved in:
| Main Author: | |
|---|---|
| Corporate Author: | |
| Other Authors: | |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1954.
|
| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
3120. |
| Subjects: |
PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/3120
|
|---|---|
| Y 3.N 21/5:6/3120 | Available Place a Hold |