SearchWorks (SUL) Search Results

1. Experimental and theoretical studies of axisymmetric free jets

Published:: 1959
At the Library:: SAL3 (off-campus storage) » See related record(s) to request item » NASA TR R-6 must be paged/requested
Format:: Book

2. Stagnation-point shielding by melting and vaporization

Author/Creator:: Roberts, Leonard.
Published:: 1959
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Format:: Book

3. A Theoretical study of stagnation-point ablation

Author/Creator:: Roberts, Leonard.
Published:: 1959
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Format:: Book

4. Analytic study of induced pressure on long bodies of revolution with varying nose bluntness at hypersonic speeds

Author/Creator:: Van Hise, Vernon.
Published:: 1960
At the Library:: SAL3 (off-campus storage) » See related record(s) to request item » NASA TR R-78 must be paged/requested
Format:: Book

5. Effect of aerodynamic heating on the flutter of a rectangular wing at a mach number of 2

Author/Creator:: Runyan, Harry L.
Published:: 1960
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Format:: Book

6. Investigation of the flow over simple bodies at Mach numbers of the order of 20

Author/Creator:: Henderson, Arthur.
Published:: 1960
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Format:: Book

7. Aerodynamic characteristics of a powered semispan tilting-shrouded-propeller VTOL model in hovering and transition flight

Author/Creator:: Goodson, Kenneth W.
Published:: 1962
At the Library:: SAL3 (off-campus storage) » See related record(s) to request item » NASA TN D-981 must be paged/requested
Online:: ntrs.nasa.gov
Format:: Book

8. Aerodynamic interaction effects ahead of rectangular sonic jets exhausting perpendicularly from a flat plate into a Mach number 6 free stream

Author/Creator:: Romeo, David J.
Published:: 1963
At the Library:: SAL3 (off-campus storage) » See related record(s) to request item » NASA TN D-1800 must be paged/requested
Format:: Book

9. Analysis of the effect of altimeter-system accuracy on collision probability

Author/Creator:: Gracey, William, 1913-
Published:: 1963
At the Library:: SAL3 (off-campus storage) » See related record(s) to request item » NASA TN D-1627 must be paged/requested
Format:: Book

10. Effects of rounding corners and leading edges on the windward-surface pressures of a delta wing swept 65⁰ at a Mach number of 5.96 at angles of attack from 65⁰ to 115⁰ and angles of roll from o⁰ to 25⁰ at 90⁰ angle of attack

Author/Creator:: Goldberg, Theodore J.
Published:: 1963
At the Library:: SAL3 (off-campus storage) » See related record(s) to request item » NASA TN D-1959 must be paged/requested
Format:: Book

11. Experimental and theoretical studies of the effects of camber and twist on the aerodynamic characteristics of parawings having normal aspect ratios of 3 and 6

Author/Creator:: Polhamus, Edward C. (Edward Charles), 1923-
Published:: 1963
At the Library:: SAL3 (off-campus storage) » See related record(s) to request item » NASA TN D-972 must be paged/requested
Format:: Book

12. Experimental pressures and turbulent heat-transfer coefficients associated with sinusoidal protuberances on a flat plate at a Mach number of 3

Author/Creator:: Shore, Charles P.
Published:: 1963
At the Library:: SAL3 (off-campus storage) » See related record(s) to request item » NASA TN D-1626 must be paged/requested
Format:: Book

13. An experimental study of the behavior of spheres ablating under constant aerodynamic conditions

Author/Creator:: Howell, Robert R.
Published:: 1963
At the Library:: SAL3 (off-campus storage) » See related record(s) to request item » NASA TN D-1635 must be paged/requested
Format:: Book

14. Investigation of the skid-rocker landing characteristics of spacecraft models

Author/Creator:: Stubbs, Sandy M.
Published:: 1963
At the Library:: SAL3 (off-campus storage) » See related record(s) to request item » NASA TN D-1624 must be paged/requested
Format:: Book

15. Low-speed investigation of the effects of wing sweep on the aerodynamic characteristics of parawings having equal-length leading edges and keel

Author/Creator:: Naeseth, Rodger L.
Published:: 1963
At the Library:: SAL3 (off-campus storage) » See related record(s) to request item » NASA TN D-1957 must be paged/requested
Format:: Book

16. Pressure and heat-transfer measurements on the flat face of a blunted 10 ̊half-cone body (semidisk) at a Mach number of 6.15

Author/Creator:: Stainback, P. Calvin.
Published:: 1963
At the Library:: SAL3 (off-campus storage) » See related record(s) to request item » NASA TN D-1628 must be paged/requested
Format:: Book

17. Pressure distributions on three rigid wings simulating parawings with varied canopy curvature and leading-edge sweep at Mach numbers from 2.29 to 4.65

Author/Creator:: Fournier, Paul G.
Published:: 1963
At the Library:: SAL3 (off-campus storage) » See related record(s) to request item » NASA TN D-1618 must be paged/requested
Format:: Book

18. Reynolds number effects on the induced pressures of cylindrical bodies with different nose shapes and nose drag coefficients in helium at a Mach number of 24

Author/Creator:: Wagner, Richard D., Jr.
Published:: 1963
At the Library:: SAL3 (off-campus storage) » See related record(s) to request item » NASA TR R-182 must be paged/requested
Format:: Book

19. Surface pressure distributions induced on a flat plate by a cold air jet issuing perpendicularly from the plate and normal to a low-speed free-stream flow

Author/Creator:: Vogler, Raymond D.
Published:: 1963
At the Library:: SAL3 (off-campus storage) » See related record(s) to request item » NASA TN D-1629 must be paged/requested
Format:: Book

20. Theoretical stability analysis of skid-rocker landings of space vehicles

Author/Creator:: Fralich, Robert W. (Robert William), 1924-
Published:: 1963
At the Library:: SAL3 (off-campus storage) » See related record(s) to request item » NASA TN D-1625 must be paged/requested
Format:: Book

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1. Experimental and theoretical studies of axisymmetric free jets

2. Stagnation-point shielding by melting and vaporization

3. A Theoretical study of stagnation-point ablation

4. Analytic study of induced pressure on long bodies of revolution with varying nose bluntness at hypersonic speeds

5. Effect of aerodynamic heating on the flutter of a rectangular wing at a mach number of 2

6. Investigation of the flow over simple bodies at Mach numbers of the order of 20

7. Aerodynamic characteristics of a powered semispan tilting-shrouded-propeller VTOL model in hovering and transition flight

8. Aerodynamic interaction effects ahead of rectangular sonic jets exhausting perpendicularly from a flat plate into a Mach number 6 free stream

9. Analysis of the effect of altimeter-system accuracy on collision probability

10. Effects of rounding corners and leading edges on the windward-surface pressures of a delta wing swept 65⁰ at a Mach number of 5.96 at angles of attack from 65⁰ to 115⁰ and angles of roll from o⁰ to 25⁰ at 90⁰ angle of attack

11. Experimental and theoretical studies of the effects of camber and twist on the aerodynamic characteristics of parawings having normal aspect ratios of 3 and 6

12. Experimental pressures and turbulent heat-transfer coefficients associated with sinusoidal protuberances on a flat plate at a Mach number of 3

13. An experimental study of the behavior of spheres ablating under constant aerodynamic conditions

14. Investigation of the skid-rocker landing characteristics of spacecraft models

15. Low-speed investigation of the effects of wing sweep on the aerodynamic characteristics of parawings having equal-length leading edges and keel

16. Pressure and heat-transfer measurements on the flat face of a blunted 10 ̊half-cone body (semidisk) at a Mach number of 6.15

17. Pressure distributions on three rigid wings simulating parawings with varied canopy curvature and leading-edge sweep at Mach numbers from 2.29 to 4.65

18. Reynolds number effects on the induced pressures of cylindrical bodies with different nose shapes and nose drag coefficients in helium at a Mach number of 24

19. Surface pressure distributions induced on a flat plate by a cold air jet issuing perpendicularly from the plate and normal to a low-speed free-stream flow

20. Theoretical stability analysis of skid-rocker landings of space vehicles