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Nathaniel B. Cohen
Observed names:
Cohen, N. B.,
Cohen, Nathaniel B,
Cohen, Nathaniel B.,
Cohen, Nathaniel B. (Nathaniel Bernard)
Observed institutions:
Langley Research Center,
National Aeronautics and Space Administration,
Langley Memorial Aeronautical Laboratory
OpenAlex ID:
A5037265510
Boundary-Layer Similar Solutions for Equilibrium Dissociated Air and Application to the Calculation of Laminar Heat-Transfer Distribution on Blunt Bodies in High-Speed Flow
1961
·
I. E. Beckwith
, Nathaniel B. Cohen
·
NASA Technical Reports Server (NASA)
·
23
A Theory for Predicting the Flow of Real Gases in Shock Tubes with Experimental Verification
1955
·
Robert L Trimpi
, Nathaniel B. Cohen
·
NASA STI Repository (National Aeronautics and Space Administration)
·
20
A Method for Computing Turbulent Heat Transfer in the Presence of a Streamwise Pressure Gradient for Bodies in High-Speed Flow
1959
·
Nathaniel B. Cohen
·
NASA Technical Reports Server (NASA)
·
10
PDF
A power-series solution for the unsteady laminar boundary-layer flow in an expansion wave of finite width moving through a gas initially at rest
1957
·
Nathaniel B. Cohen
·
NASA STI Repository (National Aeronautics and Space Administration)
·
9
PDF
A Nonlinear Theory for Predicting the Effects of Unsteady Laminar, Turbulent, or Transitional Boundary Layers on the Attenuation of Shock Waves in a Shock Tube with Experimental Comparison
1958
·
Robert L Trimpi
, Nathaniel B. Cohen
·
7
Hypersonic aircraft technology and applications
1970
·
Nathaniel B. Cohen
, A. J. Eggers
, et al.
·
NASA Technical Reports Server (NASA)
·
5
Aerodynamic and Heating Problems of Advanced Reentry Vehicles
1962
·
Robert L Trimpi
, Frederick C. Grant
, et al.
·
NASA Special Publication
·
5
An integral solution to the flat-plate laminar boundary-layer flow existing inside and after expansion waves and after shock waves moving into quiescent fluid with particular application to the complete shock-tube flow
1957
·
Robert L Trimpi
, Nathaniel B. Cohen
·
5
Progress and problems in atmosphere entry.
1965
·
Nathaniel B. Cohen
, A. J. Eggers
·
NASA Technical Reports Server (NASA)
·
1
PDF
Generic results of the space physics community survey
1993
·
Rikhi R. Sharma
, Nathaniel B. Cohen
·
NASA Technical Reports Server (NASA)
PDF
PROGRESS AND PROBLEIlS II? ATT.IOSPHERE ENTRY
1965
·
Alfred J. Egl
, Nathaniel B. Cohen
·
NASA Technical Reports Server (NASA)
The effect of real-air properties upon aerodynamic forces, moments, and heat transfer rates for reentry vehicles
1960
·
Nathaniel B. Cohen
, I. E. Beckwith
, et al.
·
NASA Technical Reports Server (NASA)
NACA Technical Notes
1957
·
Cohen, Nathaniel B.
·
University of North Texas Digital Library (University of North Texas)
PDF
Effect of Several Modifications to Center Body and Cowling on Supercritical Performance of a Supersonic Inlet at Mach Number of 2.02
1955
·
Robert L Trimpi
, Nathaniel B. Cohen
·
NASA STI Repository (National Aeronautics and Space Administration)
NACA Technical Notes
1955
·
Trimpi, Robert L.
, Cohen, Nathaniel B.
·
University of North Texas Digital Library (University of North Texas)
PDF
NACA Research Memorandums
1953
·
Trimpi, Robert L.
, Cohen, Nathaniel B.
·
University of North Texas Digital Library (University of North Texas)
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Works count:
24
Citation count:
85
H-index:
5
I10-index:
3
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