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supersonic aircraft

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View Lateral-directional eigenvector flying qualities guidelines for high performance aircraft By John B. Davidson

Lateral-directional eigenvector flying qualities guidelines for high performance aircraft

Lateral-directional eigenvector flying qualities guidelines for high performance aircraft

By John B. Davidson

View Supersonic wing and wing-body shape optimization using an adjoint formulation By James Reuther

Supersonic wing and wing-body shape optimization using an adjoint formulation

Supersonic wing and wing-body shape optimization using an adjoint formulation

By James Reuther

View Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets By Charles J. Trefny

Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets

Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets

By Charles J. Trefny

View Evaluation of frameworks for HSCT design optimization By Ramki Krishnan

Evaluation of frameworks for HSCT design optimization

Evaluation of frameworks for HSCT design optimization

By Ramki Krishnan

View Full flight envelope direct thrust measurement on a supersonic aircraft By Timothy R. Conners

Full flight envelope direct thrust measurement on a supersonic aircraft

Full flight envelope direct thrust measurement on a supersonic aircraft

By Timothy R. Conners

View Supersonic jet exhaust noise investigation By P. R. Knott

Supersonic jet exhaust noise investigation

Supersonic jet exhaust noise investigation

By P. R. Knott

View Development of techniques for the in situ observation of OH and HO₂ for studies of the impact of high-altitude supersonic aircraft on the stratosphere By James G. Anderson

Development of techniques for the in situ observation of OH and HO₂ for studies of the impact of high-altitude supersonic aircraft on the stratosphere

Development of techniques for the in situ observation of OH and HO₂ for studies of the impact of high-altitude supersonic aircraft on the stratosphere

By James G. Anderson

View Proceedings By Conference on Sonic Boom Research Washington, D.C. 1968.

Proceedings

Proceedings

By Conference on Sonic Boom Research Washington, D.C. 1968.

View Assessment of NASA's aircraft noise prediction capability By Milo D. Dahl

Assessment of NASA's aircraft noise prediction capability

Assessment of NASA's aircraft noise prediction capability

By Milo D. Dahl

View Changing the landscape of civil aviation By Carol J. Russo

Changing the landscape of civil aviation

Changing the landscape of civil aviation

By Carol J. Russo

View Turbulence model comparisons for a high-speed aircraft By Melissa B. Rivers

Turbulence model comparisons for a high-speed aircraft

Turbulence model comparisons for a high-speed aircraft

By Melissa B. Rivers

View Reaktivnye samolety By
Cover of Reaktivnye samolety by

Reaktivnye samolety

By

View X-15 By Robert Godwin
Cover of X-15 by robert godwin

X-15

By Robert Godwin

View The generation and radiation of supersonic jet noise By Air Force Aero Propulsion Laboratory (U.S.)

The generation and radiation of supersonic jet noise

The generation and radiation of supersonic jet noise

By Air Force Aero Propulsion Laboratory (U.S.)

View Numerical stability and control analysis towards falling-leaf prediction capabilities of splitflow for two generic high-performance aircraft models By Eric F. Charlton

Numerical stability and control analysis towards falling-leaf prediction capabilities of splitflow for two generic high-performance aircraft models

Numerical stability and control analysis towards falling-leaf prediction capabilities of splitflow for two generic high-performance aircraft models

By Eric F. Charlton

View Supersonic aerodynamic characteristics of an advanced F-16 derivative aircraft configuration By Mike C. Fox

Supersonic aerodynamic characteristics of an advanced F-16 derivative aircraft configuration

Supersonic aerodynamic characteristics of an advanced F-16 derivative aircraft configuration

By Mike C. Fox

View The kinetic nonequilibrium processes in the internal flow and in the plume of subsonic and supersonic aircrafts By Alexander M. Starik

The kinetic nonequilibrium processes in the internal flow and in the plume of subsonic and supersonic aircrafts

The kinetic nonequilibrium processes in the internal flow and in the plume of subsonic and supersonic aircrafts

By Alexander M. Starik

View Concept development of a Mach 2.4 high-speed civil transport By Langley Research Center

Concept development of a Mach 2.4 high-speed civil transport

Concept development of a Mach 2.4 high-speed civil transport

By Langley Research Center

View The atmospheric effects of stratospheric aircraft: a current consensus By A. R. Douglass

The atmospheric effects of stratospheric aircraft: a current consensus

The atmospheric effects of stratospheric aircraft: a current consensus

By A. R. Douglass

View Manual of highspeed aircraft design. By

Manual of highspeed aircraft design.

Manual of highspeed aircraft design.

By

View A preliminary evaluation of 1. Noise, 2. Air pollution, 3. Stratospheric effects, related to SST operations By W. D. Miller

A preliminary evaluation of 1. Noise, 2. Air pollution, 3. Stratospheric effects, related to SST operations

A preliminary evaluation of 1. Noise, 2. Air pollution, 3. Stratospheric effects, related to SST operations

By W. D. Miller

View Parallelization of a parabolized Navier-Stokes solver with a design optimizer By J. M. Pallis

Parallelization of a parabolized Navier-Stokes solver with a design optimizer

Parallelization of a parabolized Navier-Stokes solver with a design optimizer

By J. M. Pallis

View Advances in experiment design for high performance aircraft By Engene A. Morelli

Advances in experiment design for high performance aircraft

Advances in experiment design for high performance aircraft

By Engene A. Morelli

View Aerodynamic characteristics of a supersonic fighter aircraft model at Mach 0.40 to 2.47 By Francis J. Capone

Aerodynamic characteristics of a supersonic fighter aircraft model at Mach 0.40 to 2.47

Aerodynamic characteristics of a supersonic fighter aircraft model at Mach 0.40 to 2.47

By Francis J. Capone