J. L. Hunt

发表

Comment on ''measurement of aerodynamic heating of wind-tunnel models by means of temperature- sensitive paint.''

J. L. Hunt, R. A. Jones, 1966 .

J-F Niceron's La Perspective Curieuse Revisited

J. L. Hunt, 2006 .

Measurements of mutual interference heating for a probe antenna mounted on an Apollo reentry configuration

J. L. Hunt, R. A. Jones, 1969 .

Development and calibration of an on-line aerosol monitor for PHEBUS test FPT1

M. H. Sprenger, J. L. Hunt, J. E. OBrien, 1994 .

Heating and flow-field studies on a straight-wing hypersonic reentry vehicle at angles of attack from 20 to 80 deg with simulation of real-gas trends

J. L. Hunt, J. Hunt, 1973 .

Application of phase-change technique to thin sections with heating on both surfaces

J. I. Pitts, J. L. Hunt, C. B. Richie, 1973 .

Scramjet exhaust simulation technique for hypersonic aircraft nozzle design and aerodynamic tests

N. A. Talcott, J. L. Hunt, J. M. Cubbage, 1977 .

The Guelph‐Waterloo‐McMaster interactive video‐link

J. L. Hunt, 2008 .

Performance Potential and Research Needs of a Hypersonic, Airbreathing, Lifting Missile Concept

P. L. Lawing, J. L. Hunt, D. C. Marcum, 1979 .

Hypersonic airbreathing missile concepts under study at NASA Langley Research Center

James L. Dillon, J. L. Hunt, Don C. Marcum, 1982 .

Effects of several ramp-fairing, umbilical, and pad configurations on aerodynamic heating to Apollo command module at Mach 8

J. L. Hunt, R. A. Jones, 1968 .

Conceptual study of hypersonic airbreathing missiles

P. L. Lawing, J. L. Hunt, D. C. Marcum, 1978 .

A second bibliography on collision-induced absorption

J. L. Hunt, J. D. Poll, J. Hunt, 1986 .

Thin wing corrections for phase-change heat-transfer data.

J. I. Pitts, J. L. Hunt, J. Hunt, 1971 .

Heat transfer to the windward side of a fineness-ratio-2.9 cylinder with nearly spherical ends at a Mach number of 6 and angles of attack of 50 deg, 70 deg, and 90 deg

J. L. Hunt, 1969 .

Streamtube analysis of a hydrogen-burning scramjet exhaust and simulation technique

N. A. Talcott, J. L. Hunt, 1977 .

Workshop Report: Infrared Absorption in Compressed Gases

J. L. Hunt, J. D. Poll, 1985 .

Hypersonic Airbreathing Missile

P. L. Lawing, J. L. Hunt, D. C. Marcum, 1978 .

Use of fusible temperature indicators for obtaining quantitative aerodynamic heat-transfer data

J. L. Hunt, J. Hunt, R. A. Jones, 1966 .

Aerodynamic heat transfer to a hypersonic research aircraft model /X-24C/ at Mach 6

P. L. Lawing, J. L. Hunt, 1976 .

Use of tetrafluoromethane to simulate real-gas effects on the hypersonic aerodynamics of blunt vehicles

J. L. Hunt, R. A. Jones, J. Hunt, 1969 .

Experimental flow field and heat-transfer investigation of several tension shell configurations at a Mach number of 8

D. M. Bushnell, J. L. Hunt, R. A. Jones, 1967 .

Use of temperature-sensitive coatings for obtaining quantitative aerodynamic heat- transfer data

J. L. Hunt, R. A. Jones, 1964 .

NASA's hypersonic fluid and thermal physics program (Aerothermodynamics)

J. L. Hunt, R. A. Graves, 1985 .