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aerodynamics supersonic

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View Supersonic flow and shock waves By Richard Courant
Cover of Supersonic flow and shock waves by richard courant

Supersonic flow and shock waves

By Richard Courant

View Gas dynamic discontinuities By Wallace Dean Hayes

Gas dynamic discontinuities

Gas dynamic discontinuities

By Wallace Dean Hayes

View Hochgeschwindigkeits-Aerodynamik By F. Dubs
Cover of Hochgeschwindigkeits-Aerodynamik by f. dubs

Hochgeschwindigkeits-Aerodynamik

By F. Dubs

View Calculation of two-dimensional inlet flow fields by an implicit method including viscous effects - program documentation and test case By Sedat Biringen

Calculation of two-dimensional inlet flow fields by an implicit method including viscous effects - program documentation and test case

Calculation of two-dimensional inlet flow fields by an implicit method including viscous effects - program documentation and test case

By Sedat Biringen

View 1998 NASA High-Speed Research Program Aerodynamic Performance Workshop By NASA High-Speed Research Program Aerodynamic Performance Workshop (1998 Los Angeles, Calif.)

1998 NASA High-Speed Research Program Aerodynamic Performance Workshop

1998 NASA High-Speed Research Program Aerodynamic Performance Workshop

By NASA High-Speed Research Program Aerodynamic Performance Workshop (1998 Los Angeles, Calif.)

View Calculation of three-dimensional, inviscid supersonic, steady flows By Gino Moretti

Calculation of three-dimensional, inviscid supersonic, steady flows

Calculation of three-dimensional, inviscid supersonic, steady flows

By Gino Moretti

View 1999 NASA High-Speed Research Program Aerodynamic Performance Workshop By NASA High-Speed Research Program Aerodynamic Performance Workshop (1999 Anaheim, Calif.)

1999 NASA High-Speed Research Program Aerodynamic Performance Workshop

1999 NASA High-Speed Research Program Aerodynamic Performance Workshop

By NASA High-Speed Research Program Aerodynamic Performance Workshop (1999 Anaheim, Calif.)

View Application of a two-dimensional unsteady viscous analysis code to a supersonic throughflow fan stage By Ronald J. Steinke

Application of a two-dimensional unsteady viscous analysis code to a supersonic throughflow fan stage

Application of a two-dimensional unsteady viscous analysis code to a supersonic throughflow fan stage

By Ronald J. Steinke

View Chasing the demon By Dan Hampton
Cover of Chasing the demon by dan hampton

Chasing the demon

By Dan Hampton

View Higher Approximations in Aerodynamic Theory By M. J. Lighthill

Higher Approximations in Aerodynamic Theory

Higher Approximations in Aerodynamic Theory

By M. J. Lighthill

View Aerodynamic Components of Aircraft at High Speeds By Allen F. Donovan
Cover of Aerodynamic Components of Aircraft at High Speeds by allen f. donovan

Aerodynamic Components of Aircraft at High Speeds

By Allen F. Donovan

View A multi-domain spectral method for supersonic reactive flows By Wai-Sun Don

A multi-domain spectral method for supersonic reactive flows

A multi-domain spectral method for supersonic reactive flows

By Wai-Sun Don

View Longitudinal and lateral-directional aerodynamic characteristics of a wing-cone configuration at Mach numbers from 2.5 to 4.5 By Peter F. Covell

Longitudinal and lateral-directional aerodynamic characteristics of a wing-cone configuration at Mach numbers from 2.5 to 4.5

Longitudinal and lateral-directional aerodynamic characteristics of a wing-cone configuration at Mach numbers from 2.5 to 4.5

By Peter F. Covell

View Investigation of leading-edge flap performance on delta and double-delta wings at supersonic speeds By Peter F. Covell

Investigation of leading-edge flap performance on delta and double-delta wings at supersonic speeds

Investigation of leading-edge flap performance on delta and double-delta wings at supersonic speeds

By Peter F. Covell

View Applied Computational Aerodynamics By Russell M. Cummings,Scott A. Morton,William H. Mason,David R. McDaniel

Applied Computational Aerodynamics

Applied Computational Aerodynamics

By Russell M. Cummings,Scott A. Morton,William H. Mason,David R. McDaniel

View Wing theory in supersonic flow By Elie Carafoli

Wing theory in supersonic flow

Wing theory in supersonic flow

By Elie Carafoli

View Turbulent shear layers in supersonic flow By Alexander J. Smits
Cover of Turbulent shear layers in supersonic flow by alexander j. smits

Turbulent shear layers in supersonic flow

By Alexander J. Smits

View Navier-Stokes and Euler solutions for lee-side flows over supersonic delta wings By S. Naomi McMillin

Navier-Stokes and Euler solutions for lee-side flows over supersonic delta wings

Navier-Stokes and Euler solutions for lee-side flows over supersonic delta wings

By S. Naomi McMillin

View Progress in supersonic cruise aircraft technology By Cornelius Driver

Progress in supersonic cruise aircraft technology

Progress in supersonic cruise aircraft technology

By Cornelius Driver

View A computational system for aerodynamic design and analysis of supersonic aircraft By W. D. Middleton

A computational system for aerodynamic design and analysis of supersonic aircraft

A computational system for aerodynamic design and analysis of supersonic aircraft

By W. D. Middleton

View Effect of leading-edge load constraints on the design and performance of supersonic wings By Christine M. Darden

Effect of leading-edge load constraints on the design and performance of supersonic wings

Effect of leading-edge load constraints on the design and performance of supersonic wings

By Christine M. Darden

View Supersonic axial-force characteristics of a rectangular-box cavity with various length-to-depth ratios in a flat plate By A. B. Blair

Supersonic axial-force characteristics of a rectangular-box cavity with various length-to-depth ratios in a flat plate

Supersonic axial-force characteristics of a rectangular-box cavity with various length-to-depth ratios in a flat plate

By A. B. Blair

View Wind-tunnel investigation at supersonic speeds of a canard-controlled missile with fixed and free-rolling tail fins By A. B. Blair

Wind-tunnel investigation at supersonic speeds of a canard-controlled missile with fixed and free-rolling tail fins

Wind-tunnel investigation at supersonic speeds of a canard-controlled missile with fixed and free-rolling tail fins

By A. B. Blair

View A study of the sonic-boom characteristics of a blunt body at a Mach number of 6 By George C. Ashby

A study of the sonic-boom characteristics of a blunt body at a Mach number of 6

A study of the sonic-boom characteristics of a blunt body at a Mach number of 6

By George C. Ashby