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Showing 1 - 10 of 81 results
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Two-dimensional aerodynamic characteristics of the OLS/TAAT airfoil
Joyner Library
- Microforms B300
Call Number:
NAS 1.15:89435
A recontoured, upper surface designed to increase the maximum lift coefficient of a modified NACA 65 (0.82) (9.9) airfoil section
Joyner Library
- Microforms B300
Call Number:
NAS 1.15:85855
Aerodynamic characteristics and pressure distributions for an executive-jet baseline airfoil section
Joyner Library
- Microforms B300
Call Number:
NAS 1.15:4529
On the flow processes in sharply inclined and stalled airfoils in parallel movement and rotation
Joyner Library
- Microforms B300
Call Number:
NAS 1.15:77509
Flight Mechanics/Estimation Theory Symposium, 1989
Joyner Library
- Microforms B300
Call Number:
NAS 1.55:3050
Icing test results on an advanced two-dimensional high-lift multi-element airfoil
Joyner Library
- Microforms B300
Call Number:
NAS 1.15:106620
The elements of aerofoil and airscrew theory
Joyner Library
- General Stacks
Call Number:
TL574.A4 G6 1947
Tests of a NACA 65₁-213 airfoil in the NASA Langley 0.3 meter transonic cryogenic tunnel
Joyner Library
- Microforms B300
Call Number:
NAS 1.15:85732
Transonic calculation of airfoil stability and response with active controls
Joyner Library
- Microforms B300
Call Number:
NAS 1.15:85770