SearchWorks (SUL) Search Results

1. Aerodynamic effects caused by icing of an unswept NACA 65A004 airfoil

Author/Creator:: Gray, Vernon H.
Published:: 1958
At the Library:: SAL3 (off-campus storage) » See related record(s) to request item » NACA TN 4155 must be paged/requested
Format:: Book

2. Comparison of shock-expansion theory with experiment for the lift, drag, and pitching-moment characteristics of two wing-body combinations at M = 5.0

Author/Creator:: Savin, Raymond C.
Published:: 1958
At the Library:: SAL3 (off-campus storage) » See related record(s) to request item » NACA TN 4385 must be paged/requested
Format:: Book

3. Exploratory wind-tunnel investigation at high subsonic and transonic speeds of jet flaps on unswept rectangular wings

Author/Creator:: Lockwood, Vernard E.
Published:: 1958
At the Library:: SAL3 (off-campus storage) » See related record(s) to request item » NACA TN 4353 must be paged/requested
Format:: Book

4. Exploratory wind-tunnel investigation to determine the lift effects of blowing over flaps from nacelles mounted above the wings

Author/Creator:: Riebe, John M.
Published:: 1958
At the Library:: SAL3 (off-campus storage) » See related record(s) to request item » NACA TN 4298 must be paged/requested
Format:: Book

5. Investigation of minimum drag and maximum lift-drag ratios of several wing-body combinations including a cambered triangular wing at low Reynolds numbers and at supersonic speeds

Author/Creator:: Brown, Clinton E.
Published:: 1958
At the Library:: SAL3 (off-campus storage) » See related record(s) to request item » NACA TN 4020 must be paged/requested
Format:: Book

6. Lift and moment on thin arrowhead wings with supersonic edges oscillating in symmetric flapping and roll and application to the flutter of an all-movable control surface

Author/Creator:: Cunningham, H. J.
Published:: 1958
At the Library:: SAL3 (off-campus storage) » See related record(s) to request item » NACA TN 4189 must be paged/requested
Format:: Book

7. Effect of spanwise variations in gust intensity on the lift due to atmospheric turbulence

Author/Creator:: Diederich, Franklin W.
Published:: 1957
At the Library:: SAL3 (off-campus storage) » See related record(s) to request item » NACA TN 3920 must be paged/requested
Format:: Book

8. Investigation of the effects of leading-edge chord-extensions and fences in combination with leading-edge flaps on the aerodynamic characteristics at Mach numbers from 0.40 to 0.93 of a 45 degree sweptback wing at aspect ratio 4

Author/Creator:: Spreeman, Kenneth P.
Published:: 1957
At the Library:: SAL3 (off-campus storage) » Stacks » NACA TN 3845 must be paged/requested
Format:: Book

9. Lift and moment responses to penetration of sharp-edged traveling gusts, with application to penetration of weak blast waves

Author/Creator:: Drischler, Joseph A.
Published:: 1957
At the Library:: SAL3 (off-campus storage) » See related record(s) to request item » NACA TN 3956 must be paged/requested
Format:: Book

10. Approximate indicial lift functions for several wings of finite span in incompressible flow as obtained from oscillatory lift coefficients

Author/Creator:: Drischler, Joseph A.
Published:: 1956
At the Library:: SAL3 (off-campus storage) » See related record(s) to request item » NACA TN 3639 must be paged/requested
Format:: Book

11. Calculation and compilation of the unsteady-lift functions for a rigid wing subjected to sinusoidal gusts and to sinusoidal sinking oscillations

Author/Creator:: Drischler, Joseph A.
Published:: 1956
At the Library:: SAL3 (off-campus storage) » See related record(s) to request item » NACA TN 3748 must be paged/requested
Format:: Book

12. Effect of pneumatic de-icers and ice formations on aerodynamic characteristics of an airfoil

Author/Creator:: Bowden, Dean T.
Published:: 1956
At the Library:: SAL3 (off-campus storage) » Stacks » NACA TN 3564 must be paged/requested
Format:: Book

13. Linearized lifting-surface and lifting-line evaluations of sidewash behind rolling triangular wings at supersonic speeds

Author/Creator:: Bobbitt, Percey J.
Published:: 1956
At the Library:: SAL3 (off-campus storage) » See related record(s) to request item » NACA TN 3609 must be paged/requested
Format:: Book

14. Theoretical lift due to wing incidence of slender wing-body-tail combinations at zero angle of attack

Author/Creator:: Sacks, Alvin H.
Published:: 1956
At the Library:: SAL3 (off-campus storage) » See related record(s) to request item » NACA TN 3796 must be paged/requested
Format:: Book

15. Theoretical pressure distributions for some slender wing-body combinations at zero lift

Author/Creator:: Byrd, Paul F.
Published:: 1956
At the Library:: SAL3 (off-campus storage) » See related record(s) to request item » NACA TN 3674 must be paged/requested
Format:: Book

16. Effects of sweep on the maximum-lift characteristics of four aspect-ratio-4 wings at transonic speeds

Author/Creator:: Turner, Thomas R.
Published:: 1955
At the Library:: SAL3 (off-campus storage) » See related record(s) to request item » NACA TN 3468 must be paged/requested
Format:: Book

17. Hovering flight tests of a four-engine-transport vertical take-off airplane model utilizing a large flap and extensible vanes for redirecting the propeller slipstream

Author/Creator:: Tosti, Louis P.
Published:: 1955
At the Library:: SAL3 (off-campus storage) » Stacks » NACA TN 3440 must be paged/requested
Format:: Book

18. A limited flight investigation of the effect of three vortex-generator configurations on the effectiveness of a plain flap on an unswept wing

Author/Creator:: Morris, Garland J.
Published:: 1955
At the Library:: SAL3 (off-campus storage) » See related record(s) to request item » NACA TN 3536 must be paged/requested
Format:: Book

19. A note on the drag due to lift of rectangular wings of low aspect

Author/Creator:: Polhamus, Edward C.
Published:: 1955
At the Library:: SAL3 (off-campus storage) » See related record(s) to request item » NACA TN 3324 must be paged/requested
Format:: Book

20. The proper combination of lift loadings for least drag on a supersonic wing

Author/Creator:: Grant, Frederick C.
Published:: 1955
At the Library:: SAL3 (off-campus storage) » See related record(s) to request item » NACA TN 3533 must be paged/requested
Format:: Book

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1. Aerodynamic effects caused by icing of an unswept NACA 65A004 airfoil

2. Comparison of shock-expansion theory with experiment for the lift, drag, and pitching-moment characteristics of two wing-body combinations at M = 5.0

3. Exploratory wind-tunnel investigation at high subsonic and transonic speeds of jet flaps on unswept rectangular wings

4. Exploratory wind-tunnel investigation to determine the lift effects of blowing over flaps from nacelles mounted above the wings

5. Investigation of minimum drag and maximum lift-drag ratios of several wing-body combinations including a cambered triangular wing at low Reynolds numbers and at supersonic speeds

6. Lift and moment on thin arrowhead wings with supersonic edges oscillating in symmetric flapping and roll and application to the flutter of an all-movable control surface

7. Effect of spanwise variations in gust intensity on the lift due to atmospheric turbulence

8. Investigation of the effects of leading-edge chord-extensions and fences in combination with leading-edge flaps on the aerodynamic characteristics at Mach numbers from 0.40 to 0.93 of a 45 degree sweptback wing at aspect ratio 4

9. Lift and moment responses to penetration of sharp-edged traveling gusts, with application to penetration of weak blast waves

10. Approximate indicial lift functions for several wings of finite span in incompressible flow as obtained from oscillatory lift coefficients

11. Calculation and compilation of the unsteady-lift functions for a rigid wing subjected to sinusoidal gusts and to sinusoidal sinking oscillations

12. Effect of pneumatic de-icers and ice formations on aerodynamic characteristics of an airfoil

13. Linearized lifting-surface and lifting-line evaluations of sidewash behind rolling triangular wings at supersonic speeds

14. Theoretical lift due to wing incidence of slender wing-body-tail combinations at zero angle of attack

15. Theoretical pressure distributions for some slender wing-body combinations at zero lift

16. Effects of sweep on the maximum-lift characteristics of four aspect-ratio-4 wings at transonic speeds

17. Hovering flight tests of a four-engine-transport vertical take-off airplane model utilizing a large flap and extensible vanes for redirecting the propeller slipstream

18. A limited flight investigation of the effect of three vortex-generator configurations on the effectiveness of a plain flap on an unswept wing

19. A note on the drag due to lift of rectangular wings of low aspect

20. The proper combination of lift loadings for least drag on a supersonic wing