C. Hayes

发表

Aerodynamic characteristics of a series of twin-inlet air-breathing missile configurations. 2: Two-dimensional inlets at supersonic speeds

C. Hayes, 1983 .

Aerodynamic characteristics of a series of single-inlet air-breathing missile configurations

C. Hayes, 1983 .

Effect of a simulated engine jet blowing above an arrow wing at Mach 2.0

B. L. Shrout, C. Hayes, 1977 .

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. [Langley Unitary Plan wind tunnel]

J. C. Townsend, I. K. Collins, J. C. Townsend, 1979 .

Effects of simulated wing damage on the aerodynamic characteristics of a swept-wing airplane model

C. Hayes, 1968 .

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

J. C. Townsend, I. K. Collins, C. Hayes, 1979 .

Jet effects at supersonic speeds on base and afterbody pressures of a missile model having single and multiple jets

C. Hayes, N. Charczenko, N. Charczenko, 1963 .

Measurement of performance, inlet flow characteristics, and radiated noise for a turbojet engine having choked inlet flow

J. M. Cawthorn, C. Hayes, G. J. Morris, 1967 .