R. Blanchard

发表

Mars Pathfinder Entry, Descent, and Landing Reconstruction

P. Kallemeyn, R. Braun, D. Spencer, 1999 .

Mars Phoenix Entry, Descent, and Landing Trajestory and Atmosphere Reconstruction

P. Desai, R. Blanchard, 2011 .

Thermal structure of Jupiter's atmosphere near the edge of a 5‐μm hot spot in the north equatorial belt

G. Schubert, R. Blanchard, A. Seiff, 1998 .

Shuttle Orbiter Fuselage Global Temperature Measurements from Infrared Images at Hypersonic Speeds

Alan B. Tietjen, S. Berry, R. Blanchard, 2002 .

Structure of the Atmosphere of Venus up to 110 Kilometers: Preliminary Results from the Four Pioneer Venus Entry Probes

S. C. Sommer, R. Blanchard, A. Seiff, 1979, Science.

A unified form of Lambert's theorem

R. Blanchard, E. R. Lancaster, 1968 .

Three-dimensional flow simulation about the AFE vehicle in the transitional regime

Robert C. Blanchard, James N. Moss, R. Blanchard, 1989 .

Thermal Contrast in the Atmosphere of Venus: Initial Appraisal from Pioneer Venus Probe Data

S. C. Sommer, R. Blanchard, A. Seiff, 1979, Science.

Measurements of thermal structure and thermal contrasts in the atmosphere of Venus and related dynamical observations: Results From the four Pioneer Venus Probes

S. C. Sommer, Robert C. Blanchard, Donn B. Kirk, 1980 .

Shuttle high resolution accelerometer package experiment results - Atmospheric density measurements between 60 and 160 km

R. C. Blanchard, R. Blanchard, J. Nicholson, 1989 .

Shuttle Upper Atmosphere Mass Spectrometer Experimental Flight Results

R. Blanchard, J. Nicholson, T. Ozoroski, 1994 .

Orbital acceleration research experiment

D. J. Thomas, R. Blanchard, J. Nicholson, 1987 .

Rarefied-flow shuttle aerodynamics flight model

R. Blanchard, C. Moats, K. Larman, 1993 .

Venusian Probes Subsonic Drag Determination from Flight Data

W. P. Phillips, R. Blanchard, J. Findlay, 1982 .

Comparisons of subsonic drag estimates derived from Pioneer Venus probes flight data with wind-tunnel results

W. P. Phillips, R. Blanchard, J. Findlay, 1980 .

Gravity Wave Structure between 60 and 90 km Inferred from Space Shuttle Reentry Data

R. Blanchard, D. Fritts, L. Coy, 1989 .

Rarefied-flow aerodynamics measurement experiment on the Aeroassist Flight Experiment vehicle

Robert C. Blanchard, R. Blanchard, 1991 .

The Orbital Acceleration Research Experiment

D. J. Thomas, R. Blanchard, J. Nicholson, 1986 .

Free-molecule-flow force and moment coefficients of the aeroassist flight experiment vehicle

R. Blanchard, E. Hinson, 1989 .

Rarefied-flow aerodynamics measurement experiment on the aeroassist flight experiment

R. Blanchard, 1989 .

Orbiter Rarefied-Flow Reentry Measurements From the OARE on STS-62

R. Blanchard, J. Nicholson, 1995 .

Absolute acceleration measurements on STS-50 from the Orbital Acceleration Research Experiment (OARE)

R. Blanchard, J. Nicholson, James R. Ritter, 1994 .

Huygens Titan probe trajectory reconstruction using traditional methods and the program to optimize simulated trajectories II

R. Blanchard, S. Striepe, W. Fowler, 2007 .

Summary of OARE flight calibration measurements

R. Blanchard, J. Nicholson, 1995 .

Fluorometric determination of plasma 11-hydroxycorticosteroids. II. Studies on the specificity of the method.

R. Blanchard, L. E. Mejer, 1973, Clinical Chemistry.

Effect of Different Prealkalinization Concentrations of NaOH on [ 3 H ] Cortisol Recovery , in the Proposed Fluorometric Method

R. Blanchard, L. E. Mejer, 2004 .

Fluorometric determination of plasma 11-hydroxycorticosteroids. I. Rapid procedure for clinical screening.

R. Blanchard, L. E. Mejer, 1973, Clinical chemistry.

Structure of the Atmosphere of Jupiter: Galileo Probe Measurements

Frank S. Milos, Robert C. Blanchard, Donn B. Kirk, 1996, Science.

Thermal Structure of Jupiter's Upper Atmosphere Derived from the Galileo Probe

Ethiraj Venkatapathy, Frank S. Milos, Robert C. Blanchard, 1997, Science.

SOLAR CYCLE CHANGES IN INNER-ZONE PROTONS

Wilmot N. Hess, Robert C. Blanchard, R. Blanchard, 1964 .

Effect of ignition position on the run-up distance to DDT for hydrogen–air explosions

R. Blanchard, R. Grätz, Detlef Arndt, 2011 .

Explosions in closed pipes containing baffles and 90 degree bends

Rainer Grätz, Robert Blanchard, Detlef Arndt, 2010 .

Determination of atmospheric properties for STS-1 aerothermodynamic investigations

R. C. Blanchard, R. Blanchard, J. M. Price, 1981 .

Determination of the hypersonic-continuum/rarefied-flow drag coefficient of the Viking lander capsule 1 aeroshell from flight data

G. D. Walberg, R. C. Blanchard, R. Blanchard, 1980 .

Shuttle Entry Imaging Using Infrared Thermography

Scott A. Berry, Thomas J. Horvath, Martin Ross, 2007 .

Rarefied Transitional Bridging of Blunt Body Aerodynamics

R. G. Wilmoth, Robert C. Blanchard, James N. Moss, 1998 .

A note on Lambert's theorem.

R. C. Blanchard, R. Blanchard, E. R. Lancaster, 1966 .

Determination of rarefied-flow aerodynamics of the Shuttle orbiter from flight measurements on STS-6 and STS-7

G. M. Buck, R. C. Blanchard, R. Blanchard, 1985 .

The Shuttle Upper Atmosphere Mass Spectrometer Experiment

R. Blanchard, R. Duckett, E. Hinson, 1984 .

A Shuttle Upper Atmosphere Mass Spectrometer /SUMS/ experiment

R. Blanchard, R. Duckett, E. Hinson, 1982 .

Rarefied flow lift-to-drag measurements of the Shuttle Orbiter

R. Blanchard, 1986 .

AERODYNAMIC FLIGHT MEASUREMENTS AND RAREFIED-FLOW SIMULATIONS OF MARS ENTRY VEHICLES

Richard G. Wilmoth, Robert C. Blanchard, James N. Moss, 1997 .

Mars Neutral Upper Atmosphere Temporal and Spatial Variations Discovered from the Accelerometer Science Experiment aboard Mars Reconnaissance Orbiter.

R. Blanchard, R. Zurek, R. Tolson, 2007 .