A method for designing low-drag nose-inlet--body combinations for operation at moderate supersonic speeds
Explore the source record for details and available documents.
Howell, Robert R↗
SEARCH · Engineering Papers
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.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Experimental Drag Coefficients of Round Noses with Conical Windshields at Mach Number 2.72
Explore the source record for details and available documents.
Jones, Jim J↗
Performance Characteristics of Axisymmetric Two-cone and Isentropic Nose Inlets at Mach Number 1.90
Explore the source record for details and available documents.
Conners, James F↗
Preliminary Investigation of Effect on Performance of Dividing Conical-spike Nose Inlets into Halves at Mach Numbers 1.5 to 2.0
Inserting a splitter plate in the subsonic diffuser caused a pressure-recovery loss of about 1 percent for an inlet with a long nearly constant-area throat section. The loss was due to the increased surface area. Another inlet, which had a comparatively rapid area increase immediately after the throat, experienced pressure-recovery losses of 5 and 6 percent at Mach numbers of 1.8 and 2.0, respectively, and about 1 percent at Mach 1.5.
Allen, John L↗
Fuselage Side Inlets : a Study of Some Factors Affecting Their Performance and a Comparison with Nose Inlets
Explore the source record for details and available documents.
Mossman, Emmet A↗
Limited Hydrodynamic Investigation of a 1/15-size Model of a Modified Nose-inlet Multijet Water-based Aircraft
Explore the source record for details and available documents.
Mekann, Robert E↗
An Investigation at Transonic Speeds of the Effects of Fences, Drooped Nose, and Vortex Generators on the Aerodynamic Characteristics of a Wing-fuselage Combination Having a 6-percent-thick, 45 Degree Sweptback Wing
Explore the source record for details and available documents.
Hieser, Gerald↗
Force, Moment, and Pressure Characteristics of Several Annular Nose Inlets at Mach Number 3.85
Explore the source record for details and available documents.
Conners, James F↗
Investigation of the drag of blunt-nosed bodies of revolution in free flight at Mach numbers from 0.6 to 2.3
Explore the source record for details and available documents.
Wallskog, Harvey A↗
Correlation by the hypersonic similarity rule of the pressure distributions and wave drags for minimum-drag nose shapes at zero angle of attack
Explore the source record for details and available documents.
Jorgensen, Leland H↗
Some Internal-flow Characteristics of Several Axisymmetrical NACA 1-series Nose Air Inlets at Zero Flight Speed
Explore the source record for details and available documents.
Bryan, Carroll R↗
Zero-lift Drag of Several Conical and Blunt Nose Shapes Obtained in Free Flight at Mach Numbers of 0.7 to 1.3
Explore the source record for details and available documents.
Piland, Robert O↗
Transonic-wind-tunnel Investigation of the Effects of Lip Bluntness and Shape on the Drag and Pressure Recovery of a Normal-shock Nose Inlet in a Body of Revolution
Explore the source record for details and available documents.
Olstad, Walter B↗
Free-flight Aerodynamic-heating Data to Mach Number 10.4 for a Modified Von Karman Nose Shape
Explore the source record for details and available documents.
Bland, William M , Jr↗
Exploratory Materials and Missile-nose-shape Tests in a 4,000 Degree F Supersonic Air Jet
Explore the source record for details and available documents.
Purser, Paul E↗
Static-pressure error calibrations for nose-boom airspeed installations of 17 airplanes
Explore the source record for details and available documents.
Larson, Terry J↗
Heat-transfer and Pressure Distribution on Six Blunt Noses at a Mach Number of 2
Explore the source record for details and available documents.
Carter, Howard S↗
Aerodynamic Performance of Several Techniques for Spike-position Control of a Blunt-lip Nose Inlet Having Internal Contraction; Mach Numbers of 0.63 and 1.5 to 2.0
Explore the source record for details and available documents.
Anderson, Arthur A↗