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R. P. Dengler
Observed names:
Dengler, R.,
Dengler, Richard,
R Dengler,
R. DENGLER,
R. Dengler
Observed institutions:
Rohde & Schwarz (Germany),
Glenn Research Center,
Union Carbide (United States),
Technical University of Munich
ORCID:
0000-0001-6706-8550
Observed ORCID:
0000-0001-6706-8550
OpenAlex ID:
A5067427971
Self inductance of a wire loop as a curve integral
2016
·
R. Dengler
·
Advanced Electromagnetics
·
68
PDF
Advanced secondary power system for transport aircraft
1985
·
Abraham Hoffman
, I. G. Hansen
, et al.
·
University of Michigan Library Repository
·
65
Universal amplitude ratios of critical sound attenuation
1987
·
R. Dengler
, F. Schwabl
·
The European Physical Journal B
·
29
Attenuation and Dispersion of Sound Near the Liquid-Gas Critical Point
1987
·
R Dengler
, F Schwabl
·
Europhysics Letters (EPL)
·
22
PDF
Investigation of characteristics of pressure waves generated in water filled tanks impacted by high-velocity projectiles
1965
·
R. P. Dengler
, C R Morse
, et al.
·
NASA Technical Reports Server (NASA)
·
19
Renormalization group calculation of the critical exponents for the lifshitz tricritical point
1985
·
R. Dengler
·
Physics Letters A
·
11
Another derivation of generalized Langevin equations
2015
·
Dengler, R.
·
arXiv (Cornell University)
·
10
PDF
Dynamical scaling functions for relaxational critical dynamics
1985
·
R. Dengler
, H. Iro
, et al.
·
Physics Letters A
·
9
Experimental heat transfer and flow results of a chordwise-finned turbine vane with impingement, film, and convection cooling
1972
·
J. W. Gauntner
, J. Michael Lane
, et al.
·
NASA Technical Reports Server (NASA)
·
8
PDF
Investigation of catastrophic fracturing and chemical reactivity of liquid-filled tanks when impacted by projectiles of high velocity.
1964
·
R. P. Dengler
, C R Morse
, et al.
·
NASA Technical Reports Server (NASA)
·
7
The aerodynamic design and performance of the NASA/GE E3 low pressure turbine
1984
·
D. CHERRY
, R. DENGLER
·
AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
·
6
Engine investigation of an air-cooled turbine rotor blade incorporating impingement-cooled leading edge, chordwise passages, and a slotted trailing edge
1972
·
R. P. Dengler
, F. C. Yeh
, et al.
·
NASA Technical Reports Server (NASA)
·
5
Experimental investigation of aerodynamic performance of cooled turbine vanes at gas- to collant-temperature ratios up to 2.75
1973
·
R. G. Stabe
, R. P. Dengler
·
NASA STI Repository (National Aeronautics and Space Administration)
·
4
PDF
Self evacuated multilayer insulation of lightweight prefabricated panels for cryogenic storage tanks
1968
·
R. P. Dengler
, Laura Niendorf
, et al.
·
NASA Technical Reports Server (NASA)
·
4
PDF
Aerodynamic investigation of four-vane cascade designed for turbine cooling studies Technical memorandum
1970
·
R. P. Dengler
, David G. Evans
, et al.
·
NASA Technical Reports Server (NASA)
·
3
PDF
Critical phenomena of RNA-like polymers -- a synopsis
2023
·
Dengler, R.
·
arXiv (Cornell University)
·
2
PDF
A universality class for RNA-like polymers and double polymers
2022
·
Dengler, Richard
·
arXiv (Cornell University)
·
1
PDF
Radiation heat transfer characteristics of turbine vane airfoils in a water-cooled cascade
1971
·
R. P. Dengler
, H. J. Gladden
, et al.
·
NASA Technical Reports Server (NASA)
·
1
Self-evacuated Multilayer Insulation of Lightweight Prefabricated Panels for Cryogenic Space Propulsion Vehicles
1967
·
P. PERKINS
, R. DENGLER
, et al.
·
AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference (SDM)
·
1
PDF
Small, low cost, expendable turbojet engine. 2: Performance characteristics
1976
·
R. P. Dengler
, L. E. Macioce
·
NASA STI Repository (National Aeronautics and Space Administration)
PDF
Small, low-cost, expendable turbojet engine. 1: Design, fabrication, and preliminary testing
1976
·
R. P. Dengler
, L. E. Macioce
·
NASA STI Repository (National Aeronautics and Space Administration)
Lightweight, self-evacuated insulation panels
1970
·
R. P. Dengler
, Laura Niendorf
, et al.
·
NASA Technical Reports Server (NASA)
Impact sensitivity of foam insulation in presence of liquid oxygen
1965
·
R. P. Dengler
·
NASA Technical Reports Server (NASA)
Experimental Investigation of Lithium Hydride and Water Absorbers as Possible Heat-sink Materials for Hypersonic and Reentry Vehicles
1961
·
R. P. Cochran
, R. P. Dengler
, et al.
·
NASA Technical Reports Server (NASA)
Operation of an experimental air-cooled turbojet engine at turbine-inlet temperatures from 2200 R to 2935 R
1956
·
R. P. Cochran
, R. P. Dengler
, et al.
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Works count:
26
Citation count:
269
H-index:
8
I10-index:
6
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