M. H. Bertram

448 total citations
30 papers, 345 citations indexed

About

M. H. Bertram is a scholar working on Computational Mechanics, Aerospace Engineering and Applied Mathematics. According to data from OpenAlex, M. H. Bertram has authored 30 papers receiving a total of 345 indexed citations (citations by other indexed papers that have themselves been cited), including 26 papers in Computational Mechanics, 19 papers in Aerospace Engineering and 14 papers in Applied Mathematics. Recurrent topics in M. H. Bertram's work include Fluid Dynamics and Turbulent Flows (22 papers), Gas Dynamics and Kinetic Theory (14 papers) and Computational Fluid Dynamics and Aerodynamics (12 papers). M. H. Bertram is often cited by papers focused on Fluid Dynamics and Turbulent Flows (22 papers), Gas Dynamics and Kinetic Theory (14 papers) and Computational Fluid Dynamics and Aerodynamics (12 papers). M. H. Bertram collaborates with scholars based in United States. M. H. Bertram's co-authors include A. M. Cary, I. E. Beckwith, Leonard M. Weinstein, Patrick Johnston and Jason W. Moore and has published in prestigious journals such as AIAA Journal, Journal of Spacecraft and Rockets and Journal of the aeronautical sciences. [REQUEST TITLE].

In The Last Decade

M. H. Bertram

29 papers receiving 301 citations

Peers — A (Enhanced Table)

Peers by citation overlap · career bar shows stage (early→late) cites · hero ref

Name	h						Papers	Cites
M. H. Bertram United States	13	289	186	179	50	32	30	345
B. J. GRIFFITH United States	10	168 0.6×	167 0.9×	155 0.9×	23 0.5×	15 0.5×	28	268
W. D. Goodrich United States	10	214 0.7×	228 1.2×	235 1.3×	30 0.6×	13 0.4×	29	352
T. HSIEH United States	12	332 1.1×	75 0.4×	174 1.0×	20 0.4×	14 0.4×	45	384
Albert L Braslow United States	9	384 1.3×	66 0.4×	350 2.0×	35 0.7×	22 0.7×	28	486
W. D. Harvey United States	11	279 1.0×	57 0.3×	217 1.2×	33 0.7×	27 0.8×	44	326
A. M. Cary United States	11	309 1.1×	97 0.5×	177 1.0×	31 0.6×	46 1.4×	27	344
D. V. Maddalon United States	12	280 1.0×	85 0.5×	225 1.3×	54 1.1×	18 0.6×	35	362
E. THOMPSON United States	6	321 1.1×	125 0.7×	123 0.7×	37 0.7×	20 0.6×	11	336
Michael R. Mendenhall United States	10	229 0.8×	31 0.2×	280 1.6×	18 0.4×	11 0.3×	70	328
R. E. Melnik United States	11	355 1.2×	57 0.3×	179 1.0×	19 0.4×	26 0.8×	33	381

Countries citing papers authored by M. H. Bertram

Since Specialization

Citations

This map shows the geographic impact of M. H. Bertram's research. It shows the number of citations coming from papers published by authors working in each country. You can also color the map by specialization and compare the number of citations received by M. H. Bertram with the expected number of citations based on a country's size and research output (numbers larger than one mean the country cites M. H. Bertram more than expected).

Fields of papers citing papers by M. H. Bertram

Since Specialization

Physical SciencesHealth SciencesLife SciencesSocial Sciences

This network shows the impact of papers produced by M. H. Bertram. Nodes represent research fields, and links connect fields that are likely to share authors. Colored nodes show fields that tend to cite the papers produced by M. H. Bertram. The network helps show where M. H. Bertram may publish in the future.

Co-authorship network of co-authors of M. H. Bertram

This figure shows the co-authorship network connecting the top 25 collaborators of M. H. Bertram. A scholar is included among the top collaborators of M. H. Bertram based on the total number of citations received by their joint publications. Widths of edges represent the number of papers authors have co-authored together. Node borders signify the number of papers an author published with M. H. Bertram. M. H. Bertram is excluded from the visualization to improve readability, since they are connected to all nodes in the network.

All Works

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20 of 20 papers shown

Cary, A. M. & M. H. Bertram. (1974). Engineering prediction of turbulent skin friction and heat transfer in high-speed flow. NASA Technical Reports Server (NASA). 17 indexed citations

Bertram, M. H., et al.. (1971). Alleviation of vortex-induced heating to the lee side of slender wings in hypersonic flow. AIAA Journal. 9(9). 1870–1872. 14 indexed citations

Bertram, M. H., et al.. (1967). Heat transfer to wavy wall in hypersonic flow.. AIAA Journal. 5(10). 1760–1767. 21 indexed citations

Bertram, M. H., et al.. (1967). Effect of two-dimensional multiple-wave distortions on the heat transfer to a wall in hypersonic flow.. NASA Technical Reports Server (NASA). 4 indexed citations

Bertram, M. H., et al.. (1966). Effect of geometric modifications on the maximum lift-drag ratios of slender wing-body configurations at hypersonic speeds. NASA Technical Reports Server (NASA). 2 indexed citations

Bertram, M. H.. (1966). Hypersonic laminar viscous interaction effects on the aerodynamics of two-dimensional wedge and triangular planform wings. NASA Technical Reports Server (NASA). 17 indexed citations

Bertram, M. H., et al.. (1965). Studies Relating to the Attainment of High Lift-Drag Ratios at Hypersonic Speeds. NASA Technical Reports Server (NASA). 7 indexed citations

Bertram, M. H., et al.. (1965). Recent experiments in hypersonic turbulent boundary layers. NASA Technical Reports Server (NASA). 27 indexed citations

Bertram, M. H., et al.. (1963). EFFECT OF SURFACE DISTORTIONS ON THE HEAT TRANSFER TO A WING AT HYPERSONIC SPEEDS. AIAA Journal. 1(6). 1313–1319. 26 indexed citations

10.

Bertram, M. H., et al.. (1963). The correlation of oblique shock parameters for ratios of specific heats from 5/3 with application to real gas flows. NASA Technical Reports Server (NASA). 5 indexed citations

11.

Bertram, M. H., et al.. (1963). An experimental study of the pressure and heat-transfer distribution on a 70 deg sweep slab delta wing in hypersonic flow. NASA Technical Reports Server (NASA). 16 indexed citations

12.

Bertram, M. H., et al.. (1962). The Aerodynamics of Hypersonic Cruising and Boost Vehicles. NASSP. 23. 23. 6 indexed citations

13.

Bertram, M. H., et al.. (1960). The Blunt Plate In Hypersonic Flow. NASA Technical Reports Server (NASA). 7 indexed citations

14.

Bertram, M. H.. (1959). Boundary-layer Displacement Effects in Air at Mach Numbers 6.8 and 9.6. University of North Texas Digital Library (University of North Texas). 21 indexed citations

15.

Bertram, M. H., et al.. (1958). Effects of boundary-layer displacement and leading-edge bluntness on pressure distribution, skin friction, and heat transfer of bodies at hypersonic speeds. University of North Texas Digital Library (University of North Texas). 12 indexed citations

16.

Bertram, M. H.. (1956). Exploratory investigation of boundary-layer transition on a hollow cylinder at a Mach number of 6.9. University of North Texas Digital Library (University of North Texas). 7 indexed citations

17.

Bertram, M. H., et al.. (1955). An Investigation of the Aerodynamic Characteristics of Thin Delta Wings with a Symmetrical Double-wedge Section at a Mach Number of 6.9. University of North Texas Digital Library (University of North Texas). 3 indexed citations

18.

Bertram, M. H., et al.. (1954). Investigation of the aerodynamic characteristics at high supersonic Mach numbers of a family of delta wings having double-wedge sections with the maximum thickness at 0.18 chord. University of North Texas Digital Library (University of North Texas). 3 indexed citations

19.

Bertram, M. H.. (1954). Viscous and Leading-Edge Thickness Effects on the Pressures on the Surface of a Flat Plate in Hypersonic Flow. Journal of the aeronautical sciences. [REQUEST TITLE]. 21(6). 430–431. 24 indexed citations

20.

Bertram, M. H., et al.. (1951). An Investigation of Four Wings of Square Plan Form at a Mach Number of 6.86 in the Langley 11-inch Hypersonic Tunnel. University of North Texas Digital Library (University of North Texas). 2 indexed citations

Rankless uses publication and citation data sourced from OpenAlex, an open and comprehensive bibliographic database. While OpenAlex provides broad and valuable coverage of the global research landscape, it—like all bibliographic datasets—has inherent limitations. These include incomplete records, variations in author disambiguation, differences in journal indexing, and delays in data updates. As a result, some metrics and network relationships displayed in Rankless may not fully capture the entirety of a scholar's output or impact.

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