Explore Books on
supersonic aerodynamics
1-24 of 426 Books
Supersonic flow and shock waves
By Richard Courant
High-speed research
High-speed research
By High Speed Research Program Sonic Boom Workshop (3rd 1994 Langley Research Center)
Sound barrier
By Neville Duke,Charles E. Dornbusch,Lawrence J. Paszek
Super- and hypersonic aerodynamics and heat transfer
By V. Z. Parton
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
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.)
Calculation of three-dimensional, inviscid supersonic, steady flows
Calculation of three-dimensional, inviscid supersonic, steady flows
By Gino Moretti
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.)
YF-12 Experiments Symposium
YF-12 Experiments Symposium
By YF-12 Experiments Symposium (1978 Dryden Flight Research Center)
1997 NASA High-Speed Research Program Aerodynamic Performance Workshop
1997 NASA High-Speed Research Program Aerodynamic Performance Workshop
By NASA High-Speed Research Program Aerodynamic Performance Workshop (1997 Hampton, Va.)
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
A multi-domain spectral method for supersonic reactive flows
A multi-domain spectral method for supersonic reactive flows
By Wai-Sun Don
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
Boundary-layer transition results from the F-16XL-2 supersonic laminar flow control experiment
Boundary-layer transition results from the F-16XL-2 supersonic laminar flow control experiment
By Laurie A. Marshall
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
Applied Computational Aerodynamics
Applied Computational Aerodynamics
By Russell M. Cummings,Scott A. Morton,William H. Mason,David R. McDaniel
Wing theory in supersonic flow
Wing theory in supersonic flow
By Elie Carafoli
Turbulent shear layers in supersonic flow
By Alexander J. Smits
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
Progress in supersonic cruise aircraft technology
Progress in supersonic cruise aircraft technology
By Cornelius Driver
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
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