804 total citations 28 papers, 486 citations indexed
About
Albert L Braslow is a scholar working on Computational Mechanics, Aerospace Engineering and Global and Planetary Change.
According to data from OpenAlex, Albert L Braslow has authored 28 papers receiving a total of 486 indexed citations (citations by other indexed papers that have themselves been cited), including 17 papers in Computational Mechanics, 17 papers in Aerospace Engineering and 7 papers in Global and Planetary Change. Recurrent topics in Albert L Braslow's work include Fluid Dynamics and Turbulent Flows (10 papers), Computational Fluid Dynamics and Aerodynamics (10 papers) and Advanced Aircraft Design and Technologies (7 papers). Albert L Braslow is often cited by papers focused on Fluid Dynamics and Turbulent Flows (10 papers), Computational Fluid Dynamics and Aerodynamics (10 papers) and Advanced Aircraft Design and Technologies (7 papers). Albert L Braslow collaborates with scholars based in United States. Albert L Braslow's co-authors include R. M. Hicks, F. S. Collier, D. V. Maddalon, M. Fischer, J. E. Hackett, Andrew Thomas, Albert E Von Doenhoff, Dennis M. Bushnell, William S. Saric and R. C. Lock and has published in prestigious journals such as NASA STI Repository (National Aeronautics and Space Administration), Defense Technical Information Center (DTIC) and University of North Texas Digital Library (University of North Texas).
Citations per year, relative to Albert L Braslow Albert L Braslow (= 1×)
peers
W. D. Harvey
Countries citing papers authored by Albert L Braslow
Since
Specialization
Citations
This map shows the geographic impact of Albert L Braslow'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 Albert L Braslow with the expected number of citations based on a country's size and research output (numbers larger than one mean the country cites Albert L Braslow more than expected).
Fields of papers citing papers by Albert L Braslow
This network shows the impact of papers produced by Albert L Braslow. 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 Albert L Braslow. The network helps show where Albert L Braslow may publish in the future.
Co-authorship network of co-authors of Albert L Braslow
This figure shows the co-authorship network connecting the top 25 collaborators of Albert L Braslow.
A scholar is included among the top collaborators of Albert L Braslow 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
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All Works
20 of 20 papers shown
1.
Braslow, Albert L. (2012). A History of Suction-Type Laminar - Flow Control with Emphasis on Flight Research. NASA Technical Reports Server (NASA).51 indexed citations
2.
Braslow, Albert L. (1999). History of Suction-Type Laminar-Flow Control with Emphasis on Flight Resrearch: Monographs in Aerospace History Number 13. NASA STI Repository (National Aeronautics and Space Administration).19 indexed citations
Braslow, Albert L, et al.. (1990). Applied aspects of laminar-flow technology.17 indexed citations
5.
Maddalon, D. V., et al.. (1989). Laminar-flow flight experiments.6 indexed citations
6.
Thomas, Andrew, William S. Saric, Albert L Braslow, et al.. (1985). Aircraft Drag Prediction and Reduction. Defense Technical Information Center (DTIC).15 indexed citations
7.
Braslow, Albert L & M. Fischer. (1985). Design considerations for application of laminar flow control systems to transport aircraft. NASA Technical Reports Server (NASA).7 indexed citations
Braslow, Albert L & W. J. Alford. (1972). Advanced subsonic transport technology.. 10.1 indexed citations
10.
Braslow, Albert L, et al.. (1971). Application of advanced aerodynamics to future transport aircraft. NASA Technical Reports Server (NASA). 270. 165.1 indexed citations
11.
Braslow, Albert L. (1966). A review of factors affecting boundary-layer transition. NASA Technical Reports Server (NASA).16 indexed citations
12.
Braslow, Albert L, et al.. (1966). Use of grit-type boundary-layer-transition trips on wind-tunnel models. NASA Technical Reports Server (NASA).107 indexed citations
13.
Braslow, Albert L. (1966). Analysis of boundary-layer transition on X-152-2 research airplane. NASA Technical Reports Server (NASA).2 indexed citations
14.
Braslow, Albert L, et al.. (1962). A RIGIDLY FORCED OSCILLATION SYSTEM FOR MEASURING DYNAMIC-STABILITY PARAMETERS IN TRANSONIC AND SUPERSONIC WIND TUNNELS. Defense Technical Information Center (DTIC).8 indexed citations
15.
Braslow, Albert L, et al.. (1958). Effects of surface roughness on transition. NASA Technical Reports Server (NASA).3 indexed citations
16.
Braslow, Albert L. (1958). Effect of Distributed Granular-type Roughness on Boundary-layer Transition at Supersonic Speeds with and Without Surface Cooling. University of North Texas Digital Library (University of North Texas).2 indexed citations
17.
Braslow, Albert L, et al.. (1958). Ordinates and Theoretical Pressure-distribution Data for NACA 6- and 6a-series Airfoil Sections with Thicknesses from 2 to 21 and from 2 to 15 Percent Chord, Respectively. University of North Texas Digital Library (University of North Texas).4 indexed citations
18.
Braslow, Albert L, et al.. (1958). Dynamic directional stability derivatives for a 45 degree swept-wing-vertical-tail airplane model at transonic speeds and angles of attack, with a description of the mechanism and instrumentation employed. NASA Technical Reports Server (NASA).1 indexed citations
19.
Braslow, Albert L, et al.. (1958). Simplified method for determination of critical height of distributed roughness particles for boundary-layer transition at Mach numbers from 0 to 5. University of North Texas Digital Library (University of North Texas).173 indexed citations
20.
Braslow, Albert L, et al.. (1952). Experimental study of the effects of finite surface disturbances and angle of attack on the laminar boundary layer of an NACA 64A010 airfoil with area suction. University of North Texas Digital Library (University of North Texas).4 indexed citations
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