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John P. Stack

Observed names: J. P. Stack, J. STACK, JOHN STACK, John Stack, Stack, J. P., Stack, John P.
OpenAlex ID: A5026321927
Crossflow-vortex instability and transition on a 45 deg swept wing
1989 · J. DAGENHART, J. STACK, et al. · AIAA Fluid Dynamics, Plasma Dynamics and Lasers Conference · 56
A unique measurement technique to study laminar-separation bubble characteristics on an airfoil
1987 · J. STACK, S. MANGALAM, et al. · AIAA Fluid Dynamics, Plasma Dynamics and Lasers Conference · 37
The phase reversal phenomenon at flow separation and reattachment
1988 · J. STACK, S. MANGALAM, et al. · AIAA Aerospace Sciences Meeting · 24
Tests of Airfoils Designed to Delay the Compressibility Burble
1943 · John Stack · NASA STI Repository (National Aeronautics and Space Administration) · 22
Surface hot-film method for the measurement of transition, separation and reattachment points
1993 · AKIHIKO NAKAYAMA, JOHN STACK, et al. · AIAA Fluid Dynamics, Plasma Dynamics and Lasers Conference · 21
Tests in the Variable Density Wind Tunnel to Investigate the Effects of Scale and Turbulence on Airfoil Characteristics
1931 · John Stack · NASA STI Repository (National Aeronautics and Space Administration) · 21
Tests of 16 related airfoils at high speed
1934 · John Stack, Albert E Von Doenhoff · 17
The Compressibility Burble and the Effect of Compressibility on Pressures and Forces Acting on a Airfoil
1939 · John Stack, W F Lindsey, et al. · NASA Technical Reports Server (NASA) · 15
A New Multipoint Thin-Film Diagnostic Technique for Fluid Dynamic Studies
1988 · W. G. Sewall, J. P. Stack, et al. · SAE technical papers on CD-ROM/SAE technical paper series · 14
Compressible Flows in Aeronautics
1945 · JOHN STACK · Journal of the aeronautical sciences. [REQUEST TITLE] · 11
The NACA High-Speed Wind Tunnel and Tests of Six Propeller Sections
1934 · John Stack · NASA Technical Reports Server (NASA) · 10
Simultaneous detection of separation and transition in surface shear layers
1989 · Siva Mangalam, John Stack, et al. · NASA Technical Reports Server (NASA) · 9
Experiments on a Separation Bubble Over an Eppler 387 Airfoil at Low Reynolds Numbers using Thin-Film Arrays
1990 · Marc C. Mousseux, Ndaona Chokani, et al. · Advances in soil science · 7
In-flight detection of Tollmien-Schlichting instabilities in laminar flow
1987 · C. C. Croom, Gregory S. Manuel, et al. · NASA Technical Reports Server (NASA) · 7
Tests of N-85, N-86 and N-87 Airfoil Sections in the 11-Inch High Speed Wind Tunnel
1938 · John Stack, W F Lindsey · 6
The Compressibility Burble
1935 · John Stack · NASA Technical Reports Server (NASA) · 6
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Airfoil Pressure Distribution Investigation in the Variable Density Wind Tunnel
1931 · Eastman N Jacobs, John Stack, et al. · 6
Investigation of the NACA 4-(3)(8)-045 Two-Blade Propellers at Forward Mach Numbers to 0.725 to Determine the Effects of Compressibility and Solidity on Performance
1944 · John Stack, Eugene C Draley, et al. · 5
Compressibility Effects in Aeronautical Engineering
1941 · John Stack · NASA Technical Reports Server (NASA) · 4
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Effects of Compressibility on High Speed Flight
1934 · JOHN STACK · Journal of the aeronautical sciences. [REQUEST TITLE] · 4
The NASA Langley Laminar-Flow-Control Experiment on a Swept Supercritical Airfoil: Basic Results for Slotted Configuration
1989 · C. D. Harris, Cuyler W. Brooks, et al. · NASA STI Repository (National Aeronautics and Space Administration) · 2
Characteristics of Low-Aspect-Ratio Wings at Supercritical Mach Numbers
1949 · John Stack, W F Lindsey · 2
Laminar-flow wind tunnel experiments
1989 · W. D. Harvey, C. D. Harris, et al. · NASA Technical Reports Server (NASA) · 1
Predicted and hot-film measured Tollmien-Schlichting wave characteristics
1987 · John Stack, Robert B. Yeaton, et al. · NASA Technical Reports Server (NASA) · 1
Tollmien-Schlschfing Instabilities in Laminar Flow In-Flight Detection of
1987 · Cynthia C. Croom, Gregory S. Manuel, et al. · SAE technical papers on CD-ROM/SAE technical paper series · 1
Works count: 41
Citation count: 313
H-index: 10
I10-index: 11
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