Get started
Author

CARL D. ENGEL

Observed names: C. D. ENGEL, C. D. Engel, Engel, C. D., Engel, Carl D.
OpenAlex ID: A5113813804
Transverse waves in detonations. II - structure and spacing in H sub 2-O sub 2, C sub 2 H sub 4-O sub 2, and CH sub 4-O sub 2 systems.
1969 · ROGER A. STREHLOW, CARL D. ENGEL · AIAA Journal · 147
Ablation and radiation coupled viscous hypersonic shock layers.
1973 · CARL D. ENGEL, RICHARD C. FARMER, et al. · AIAA Journal · 23
Short Duration Base Heating Test Improvements
1999 · Robert L. Bender, Mark D'Agostino, et al. · NASA STI Repository (National Aeronautics and Space Administration) · 2
PDF
Radiation absorption effects on heating loads encountered during hyperbolic entry.
1969 · C. D. ENGEL, L. W. SPRADLEY · Journal of Spacecraft and Rockets · 2
Mechanical Impact Testing: A Statistical Measurement
2013 · C. D. Engel, Stephen D. Herald, et al. · NASA Technical Reports Server (NASA) · 1
PDF
Oxygen Compatibility Testing of Composite Materials
2006 · C. D. Engel, Casey Watkins · NASA Technical Reports Server (NASA) · 1
Potential of Organic Matrix Composites for Liquid Oxygen Tank
2005 · Samuel Eddie Davis, Stephen D. Herald, et al. · NASA Technical Reports Server (NASA) · 1
Formulation, derivation and development of the analysis of the interaction of ablating protection systems and stagnation region heating
1970 · C. D. Engel, D. D. Esch, et al. · NASA Technical Reports Server (NASA) · 1
The effects of shock layer radiation and viscous coupling on the total heating rate to a reentering blunt body
1968 · C. D. Engel, L. W. Spradley · NASA Technical Reports Server (NASA) · 1
PDF
Formulation of a method for predicting coupled convective and radiative heat transfer about a blunt body
1968 · C. D. Engel, L. W. Spradley · NASA Technical Reports Server (NASA) · 1
PDF
Cycom 977-2 Composite Material: Impact Test Results
2005 · C. D. Engel, Stephen D. Herald, et al. · NASA Technical Reports Server (NASA)
Heated Promoted Combustion-Initial Test Results
2005 · C. D. Engel, Stephen D. Herald, et al. · NASA Technical Reports Server (NASA)
Standard Chemical Ignition Source Characteristics for Flammability Testing
2003 · C. D. Engel · NASA STI Repository (National Aeronautics and Space Administration)
Reference Material Kydex(registered trademark)-100 Test Data Message for Flammability Testing
2003 · C. D. Engel, E. H. Richardson, et al. · NASA Technical Reports Server (NASA)
PDF
SRB ascent aerodynamic heating design criteria reduction study, volume 1
1989 · William K. Crain, Cynthia Frost, et al. · NASA STI Repository (National Aeronautics and Space Administration)
PDF
SRB thermal environments
1989 · Crain, W. K., Knox, E. C., et al. · NASA STI Repository (National Aeronautics and Space Administration)
PDF
Orbital flight test shuttle external tank aerothermal flight evaluation, volume 2
1986 · Sarat C. Praharaj, C. D. Engel, et al. · NASA Technical Reports Server (NASA)
PDF
Orbital flight test shuttle external tank aerothermal flight evaluation, volume 3
1986 · Engel, Carl D., Praharaj, Sarat C., et al. · NASA Technical Reports Server (NASA)
Boundary layer simulator improvement
1984 · Sarat C. Praharaj, Craig P. Schmitz, et al. · NASA Technical Reports Server (NASA)
AOTV Low L/D Preliminary Aeroheating Design Environment
1983 · C. D. Engel · NASA STI Repository (National Aeronautics and Space Administration)
Wake flowfields for Jovian probe
1980 · Engel, C. D., Hair, L. M. · NASA STI Repository (National Aeronautics and Space Administration)
PDF
Tumbling-vehicle entry heating
1979 · C. D. Engel · NASA Tech Briefs
Jovian probe wake flowfield. [For the Galileo spacecraft
1979 · C. D. Engel · NASA Technical Reports Server (NASA)
Jovian probe wake flowfield
1979 · Engel, C. D. · NASA STI Repository (National Aeronautics and Space Administration)
PDF
Reentry Design Handbook for Sounding Rocket Payloads
1977 · J. V. Mcanally, C. D. Engel, et al. · Defense Technical Information Center (DTIC)
Works count: 31
Citation count: 180
H-index: 2
I10-index: 2
Year
Topic
Type