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Partner: UNT Libraries Government Documents Department

Decade: 1950-1959

Year: 1955

Collection: National Advisory Committee for Aeronautics Collection

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Effects of wing position and fuselage size on the low-speed static rolling stability characteristics of a delta-wing model

Effects of wing position and fuselage size on the low-speed static rolling stability characteristics of a delta-wing model

Arrangement of fusiform bodies to reduce the wave drag at supersonic speeds

Arrangement of fusiform bodies to reduce the wave drag at supersonic speeds

Standard atmosphere - tables and data for altitudes to 65,800 feet

Standard atmosphere - tables and data for altitudes to 65,800 feet

Investigations at supersonic speeds of 22 triangular wings representing two airfoil sections for each of 11 apex angles

Investigations at supersonic speeds of 22 triangular wings representing two airfoil sections for each of 11 apex angles

Theoretical and analog studies of the effects of nonlinear stability derivatives on the longitudinal motions of an aircraft in response to step control deflections and to the influence of proportional automatic control

Theoretical and analog studies of the effects of nonlinear stability derivatives on the longitudinal motions of an aircraft in response to step control deflections and to the influence of proportional automatic control

A unified two-dimensional approach to the calculation of three-dimensional hypersonic flows, with application to bodies of revolution

A unified two-dimensional approach to the calculation of three-dimensional hypersonic flows, with application to bodies of revolution

Transonic flow past cone cylinders

Transonic flow past cone cylinders

Quasi-cylindrical theory of wing-body interference at supersonic speeds and comparison with experiment

Quasi-cylindrical theory of wing-body interference at supersonic speeds and comparison with experiment

High-resolution autoradiography

High-resolution autoradiography

A comparison of the maneuvering performance of a monowing versus a cruciform missile

A comparison of the maneuvering performance of a monowing versus a cruciform missile

Aerodynamic characteristics of various configurations of a model of a 45 degree swept-wing airplane at a Mach number of 2.01

Aerodynamic characteristics of various configurations of a model of a 45 degree swept-wing airplane at a Mach number of 2.01

Experimental investigation of a transonic axial-flow-compressor rotor with double-circular-arc airfoil blade sections II : blade-element performance

Experimental investigation of a transonic axial-flow-compressor rotor with double-circular-arc airfoil blade sections II : blade-element performance

Design and test of mixed-flow impellers V : design procedure and performance results for two vaned diffusers tested with impeller model MFI-1B

Design and test of mixed-flow impellers V : design procedure and performance results for two vaned diffusers tested with impeller model MFI-1B

Rotating-stall and rotor-blade-vibration survey of a 13-stage axial-flow compressor in a turbojet engine

Rotating-stall and rotor-blade-vibration survey of a 13-stage axial-flow compressor in a turbojet engine

Effects of wing-mounted tank-type stores on the low lift buffeting and drag of a swept-wing airplane configuration between Mach numbers of 0.8 and 1.3

Effects of wing-mounted tank-type stores on the low lift buffeting and drag of a swept-wing airplane configuration between Mach numbers of 0.8 and 1.3

Investigation at high subsonic speeds of the effects of various underwing external-store arrangements on the aerodynamic characteristics of a 1/16-scale model of the Douglas D-558-II Research Airplane

Investigation at high subsonic speeds of the effects of various underwing external-store arrangements on the aerodynamic characteristics of a 1/16-scale model of the Douglas D-558-II Research Airplane

A flight investigation at transonic speeds of a model having a triangular wing of aspect ratio 4

A flight investigation at transonic speeds of a model having a triangular wing of aspect ratio 4

Preliminary investigation of a conical spike inlet in combination with a vertical-wedge auxiliary inlet at Mach number 1.9

Preliminary investigation of a conical spike inlet in combination with a vertical-wedge auxiliary inlet at Mach number 1.9

A study of conical camber for triangular and sweptback wings

A study of conical camber for triangular and sweptback wings

Performance of a double-cone inlet with and without a shroud at below-design Mach numbers

Performance of a double-cone inlet with and without a shroud at below-design Mach numbers

Engine performance of precision-forged, electropolished and machined blades of Nimonic 80 and 80A alloys

Engine performance of precision-forged, electropolished and machined blades of Nimonic 80 and 80A alloys

Exploratory investigation of the low-speed static stability of a configuration employing three identical triangular wing panels and a body of equal length

Exploratory investigation of the low-speed static stability of a configuration employing three identical triangular wing panels and a body of equal length

A study of the application of airfoil section data to the estimation of the high-subsonic-speed characteristics of swept wings

A study of the application of airfoil section data to the estimation of the high-subsonic-speed characteristics of swept wings

Static stability and control of canard configurations at Mach numbers from 0.70 to 2.22 : lateral-directional characteristics of a triangular wing and canard

Static stability and control of canard configurations at Mach numbers from 0.70 to 2.22 : lateral-directional characteristics of a triangular wing and canard

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