Explore Books on
supersonic aerodynamics
1-24 of 430 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
YF-12 Experiments Symposium
YF-12 Experiments Symposium
By YF-12 Experiments Symposium (1978 Dryden Flight Research Center)
Calculation of three-dimensional, inviscid supersonic, steady flows
Calculation of three-dimensional, inviscid supersonic, steady flows
By Gino Moretti
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.)
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.)
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.)
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
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
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
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
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
Tables of inviscid supersonic flow about circular cones at incidence [gamma]=1.4
Tables of inviscid supersonic flow about circular cones at incidence [gamma]=1.4
By D. J. Jones
Effect on tail-fin span on stability and control characteristics of a canard-controlled missile at supersonic Mach numbers
Effect on tail-fin span on stability and control characteristics of a canard-controlled missile at supersonic Mach numbers
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
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
Wind-tunnel investigation at supersonic speeds of a remote-controlled canard missile with a free-rolling-tail brake torque system
Wind-tunnel investigation at supersonic speeds of a remote-controlled canard missile with a free-rolling-tail brake torque system
By A. B. Blair
The natural flow wing-design concept
The natural flow wing-design concept
By Richard M. Wood
Study of lee-side flows over conically cambered delta wings at supersonic speeds
Study of lee-side flows over conically cambered delta wings at supersonic speeds
By Richard M. Wood