Explore Books on
aerodynamics supersonic.

On the flow of a compressible fluid by the hodograph method.

By Langley Aeronautical Laboratory

On the flow of a compressible fluid by the hodograph method. I- Unification and extension of present-day results

By Langley Aeronautical Laboratory

Preliminary investigation of supersonic diffusers

By Langley Aeronautical Laboratory

Summary of information on support interference at transonic and supersonic speeds

By Langley Aeronautical Laboratory

Surface pressure data on a series of analytic forebodies at Mach numbers from 1.70 to 4.50 and combined angles of attack and sideslip

By

Supersonic through-flow fan design

By

Wind-tunnel/flight correlation study of aerodynamic characteristics of a large flexible supersonic cruise airplane (XB-70-1).

By

Propulsion and airframe aerodynamic interactions of supersonic V/STOL configurations

By

Application of advanced computational codes in the design of an experiment for a supersonic throughflow fan rotor

By

Surface pressure data on a series of conical forebodies at mach numbers from 1.70 to 4.50 and combined angles of attack and sideslip

By

Wind-tunnel development on an SR-71 aerospike rocket flight test configuration

By

Review of aeronautical wind tunnel facilities

By

Coherent large-scale structures in high Reynolds number supersonic jets

By

Inlet flowfield investigation

By

Fiziko-gazodinamicheskie ballisticheskie issledovanii︠a︡

By

Evaluation of a technique to generate artificially thickened boundary layers in supersonic and hypersonic flows

By

Surface pressure data on a series of conical forebodies at mach numbers from 1.70 to 4.50 and combined angles of attack and sideslip

By

Supersonic through-flow fan design

By

Supersonic hydrogen combustion studies.

By

Surface pressure data on a series of analytic forebodies at Mach numbers from 1.70 to 4.50 and combined angles of attack and sideslip

By

Surface-pressure and flow-visualization data at mach number 1.60 for three 65p0s delta wings varying in leading-edge radius and camber

By

Wind-tunnel/flight correlation study of aerodynamic characteristics of a large flexible supersonic cruise airplane (XB-70-1).

By

Coherent large-scale structures in high Reynolds number supersonic jets

By

Supersonic combustion engine testbed

By