Comparison of the Experimental and Theoretical Distributions of Lift on a Slender Inclined Body of Revolution at M = 2
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Perkins, Edward W↗
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Turbulent Flow Through Porous Resistances Slightly Inclined to the Flow Direction
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Loeffler, Albert L , Jr↗
Estimation of the forces and moments acting on inclined bodies of revolution of high fineness ratio
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Allen, H Julian↗
Supersonic Tunnel Investigation by Means of Inclined-plate Technique to Determine Performance of Several Nose Inlets over Mach Number Range of 1.72 to 2.18
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Fox, Jerome L↗
Observations of Unsteady Flow Phenomena for an Inclined Body Fitted with Stabilizing Fins
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Mead, Merrill H↗
Buffeting of a Vertical Tail on an Inclined Body at Supersonic Mach Numbers
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Gowen, Forrest E↗
Calculation of aerodynamic forces on an inclined dual-rotating propeller
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Crigler, John L↗
Investigation of the NACA 1.167-(0)(03)-058 and NACA 1.167-(0)(05)-058 Three-blade Propellers at Forward Mach Numbers to 0.92 Including Effects of Thrust-axis Inclination
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Demele, Fred A↗
A preliminary investigation of aerodynamic characteristics of small inclined air outlets at transonic Mach numbers
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Dewey, Paul E↗
A Flight Investigation of the Effects of Inclination of the Principal Axis of Inertia on the Dynamic Lateral Stability of the Republic XF-91 Airplane
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Finch, Thomas W↗
A Study of the Effects of Body Shape on the Vortex Wakes of Inclined Bodies at a Mach Number of 2
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Gowen, Forrest E↗
Investigation of the Normal Force Accompanying Thrust-axis Inclination of the NACA 1.167-(0)(03)-058 and the NACA 1.167-(0)(05)-058 Three-blade Propellers at Forward Mach Numbers to 0.90
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Demele, Fred A↗
Forces and Moments on Inclined Bodies at Mach Numbers from 3.0 to 6.3
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Dennis, David H↗
Free-flight Determination of Force and Stability Characteristics of an Inclined Body of Fineness Ratio 16.9 at a Mach Number of 1.74
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Gillespie, Warren, Jr↗
Investigation of Some Wake Vortex Characteristics of an Inclined Ogive-cylinder Body at Mach Number 1.98
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Jorgensen, Leland H↗
Initial inclination of the mixing boundary separating an exhausting supersonic jet from a supersonic ambient stream
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Love, Eugene S↗
Investigation of Some Wake Vortex Characteristics of an Inclined Ogive-Cylinder Body at Mach Number 2
For a body consisting of a fineness-ratio-3 ogival nose tangent to a cylindrical afterbody 7.3 diameters long, pitot-pressure distributions in the flow field, pressure distributions over the body, and downwash distributions along a line through the vortex centers have been measured for angles of attack to 20 degrees. The Reynolds numbers, based on body diameter, were 0.15 x 10 to the 6th power and 0.44 x 10 to the 6th power. Comparisons of computed and measured vortex paths and downwash distributions are made. (author)
Jorgensen, Leland H↗
Determination of induced velocity in front of an inclined propeller by a magnetic-analogy method
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Lahatte, James A , Jr↗