Small-scale Transonic Investigation of a 45 Degree Sweptback Wing of Aspect Ratio 4 with Combinations of Nose-flap Deflections and Wing Twist
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Alford, William J , Jr↗
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Results for “NOSE”
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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A low-speed experimental study of the directional characteristics of a sharp-nosed fuselage through a large angle-of-attack range at zero angle of sideslip
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Letko, William↗
Investigation of Pressure Recovery of a Single-conical-shock Nose Inlet at Mach Number 5.4
An experimental investigation of the performance of a single-conical-shock diffuser was conducted at a Mach number of 5.4 and a Reynolds number based on model diameter of 375,000. Total-pressure recoveries of 13.7 and 13.1 percent were obtained at angles of attack of 0 degrees and 3 degrees, respectively. The corresponding kinetic energy efficiencies were 86.4 percent at an angle of attack of 0 degrees and 86.0 percent at an angle of attack of 3 degrees.
DIFFUSERS, SUPERSONIC↗
An Investigation at Mach Number 2.40 of Flap-type Controls Equipped with Overhang Nose Balances
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Mueller, James N↗
Preliminary investigation of the effects of several seeker-nose configurations on the longitudinal characteristics of a canard-type missile at a Mach number of 1.60
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Robins, A Warner↗
Flight Determination of Drag of Normal-shock Nose Inlets with Various Cowling Profiles at Mach Numbers from 0.9 to 1.5
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Sears, R I↗
Preliminary Investigation of the Total-pressure-recovery Characteristics of a Symmetric and Asymmetric Nose Inlet over a Wide Range of Angle of Attack at Supersonic Mach Numbers
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Carter, Howard S↗
Transonic Drag Measurements of Eight Body-nose Shapes
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Stoney, William E JR↗
Investigation of a Missile Airframe with Control Surfaces Consisting of Projecting Quadrants of the Nose Cone
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Lazzeroni, Frank A↗
Force Measurements on Cone-Cylinder Body of Revolution with Various Nose and Fin Configurations at Mach Number 4.0
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Rabb, Leonard↗
Effect of nose shape and trailing-edge bluntness on the aerodynamic characteristics of an unswept wing of aspect ratio 3.1, taper ratio 0.4, and 3-percent thickness
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Heitmeyer, John C↗
Some internal-flow characteristics at zero flight speed of an annular supersonic inlet and an open-nose inlet with sharp and rounded lips
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Milillo, Joseph R↗
Performance of Isentropic Nose Inlets at Mach Number of 5.6
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Haefeli, Rudolph C↗
Characteristics of Flow About Axially Symmetric Isentropic Spikes for Nose Inlets at Mach Number 3.85
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Connors, James F↗
Investigation of a Flow Deflector and an Auxiliary Scoop for Improving Off-design Performance of Nose Inlets
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Anderson, Warren E↗
The Effect of Lip Shape on a Nose-inlet Installation at Mach Numbers from 0 to 1.5 and a Method for Optimizing Engine-inlet Combinations
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Mossman, Emmet A↗
Flight determination of the drag of conical-shock nose inlets with various cowling shapes and axial positions of the center body at Mach numbers from 0.8 to 2.0
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Merlet, Charles, F↗
Preliminary investigation of an asymmetric swept nose inlet of circular projection at Mach number 3.85
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Connors, James F↗