Explore: Boundary Layer Control
Discover books, insights, and more — all in one place.
Learn more about Boundary Layer Control with top reads curated from trusted sources — all in one place.
AI-Generated Overview About “boundary-layer-control”:
Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1Control of flow separation
By Paul K. Chang

“Control of flow separation” Metadata:
- Title: Control of flow separation
- Author: Paul K. Chang
- Language: English
- Number of Pages: Median: 523
- Publisher: Hemisphere Pub. Co.
- Publish Date: 1976
- Publish Location: Washington
“Control of flow separation” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL5195832M
- Online Computer Library Center (OCLC) ID: 1502387
- Library of Congress Control Number (LCCN): 75017733
- All ISBNs: 9780070105133 - 0070105138
Access and General Info:
- First Year Published: 1976
- Is Full Text Available: Yes
- Is The Book Public: No
- Access Status: Borrowable
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
- Borrowing from Open Library: Borrowing link
- Borrowing from Archive.org: Borrowing link
Online Marketplaces
Find Control of flow separation at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
2The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil
By Cuyler W. Brooks
“The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil” Metadata:
- Title: ➤ The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil
- Author: Cuyler W. Brooks
- Language: English
- Number of Pages: Median: 18
- Publisher: ➤ Langley Research Center - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program - For sale by the National Technical Information Service
- Publish Date: 1989 - 1991
- Publish Location: ➤ [Washington, D.C.] - Springfield, Va - Hampton, Va
“The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil” Subjects and Themes:
- Subjects: ➤ Aerodynamics, Transonic - Aerofoils - Airfoils - Boundary layer - Boundary layer control - Drag - Drag (Aerodynamics) - Laminar boundary layer - Laminar flow - Laminar flow control - Suction - Supercritical airfoils - Supercritical wings - Swept wings - Testing - Transonic Aerodynamics
Edition Identifiers:
- The Open Library ID: ➤ OL20571034M - OL18930562M - OL17630310M - OL16132232M - OL18249910M - OL20779439M
- Online Computer Library Center (OCLC) ID: 48986179
Access and General Info:
- First Year Published: 1989
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
3Numerical simulation of the SOFIA flowfield
By Stephen P. Klotz
“Numerical simulation of the SOFIA flowfield” Metadata:
- Title: ➤ Numerical simulation of the SOFIA flowfield
- Author: Stephen P. Klotz
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - MCAT Institute - National Aeronautics and Space Administration
- Publish Date: 1994 - 1995
- Publish Location: ➤ Springfield, Va - [Washington, DC - San Jose, CA
“Numerical simulation of the SOFIA flowfield” Subjects and Themes:
- Subjects: ➤ Active control - Aerodynamic stalling - Airfoils - Boeing 747 aircraft - Boundary layer control - Cavities - Flow distribution - Leading edges - SOFIA (Airborne observatory) - Separated flow - Sound pressure - Tail assemblies - Telescopes - Unsteady flow - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL17788523M - OL17791647M - OL18081185M - OL18078541M - OL17683431M
- Online Computer Library Center (OCLC) ID: 33433883 - 32647393
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Numerical simulation of the SOFIA flowfield at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
4The boundary layer on compressor cascade blades
By Steven Deutsch
“The boundary layer on compressor cascade blades” Metadata:
- Title: ➤ The boundary layer on compressor cascade blades
- Author: Steven Deutsch
- Language: English
- Publisher: ➤ Applied Research Laboratory, The Pennsylvania State University - National Aeronautics and Space Administration
- Publish Date: 1984
- Publish Location: ➤ [Washington, D.C - State College, PA
“The boundary layer on compressor cascade blades” Subjects and Themes:
- Subjects: ➤ Airfoils - Boundary layer control - Cascades (Fluid dynamics) - Flow distribution - Laser Doppler velocimeters - Reynolds number
Edition Identifiers:
- The Open Library ID: OL17666140M - OL17727387M - OL14928515M - OL17831614M
Access and General Info:
- First Year Published: 1984
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find The boundary layer on compressor cascade blades at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
5Boundary-layer transition results from the F-16XL-2 supersonic laminar flow control experiment
By Laurie A. Marshall
“Boundary-layer transition results from the F-16XL-2 supersonic laminar flow control experiment” Metadata:
- Title: ➤ Boundary-layer transition results from the F-16XL-2 supersonic laminar flow control experiment
- Author: Laurie A. Marshall
- Language: English
- Number of Pages: Median: 48
- Publisher: ➤ NASA Center for AeroSpace Information [distributor] - National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service [distributor - Available from NASA Center for AeroSpace Information
- Publish Date: 1999
- Publish Location: ➤ Springfield, VA - Edwards, Calif - Hanover, Md - Hanover, MD
“Boundary-layer transition results from the F-16XL-2 supersonic laminar flow control experiment” Subjects and Themes:
- Subjects: ➤ Boundary layer - Boundary layer control - Boundary layer transition - F-16 (Jet fighter plane) - Laminar boundary layer - Laminar flow - Supersonic Aerodynamics
Edition Identifiers:
- The Open Library ID: OL15563026M - OL20639543M - OL17593816M - OL18139199M
- Online Computer Library Center (OCLC) ID: 43704178
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Boundary-layer transition results from the F-16XL-2 supersonic laminar flow control experiment at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
6F-16XL-2 supersonic laminar flow control flight test experiment
By Scott G. Anders
“F-16XL-2 supersonic laminar flow control flight test experiment” Metadata:
- Title: ➤ F-16XL-2 supersonic laminar flow control flight test experiment
- Author: Scott G. Anders
- Language: English
- Publisher: ➤ National Technical Information Service [distributor - National Aeronautics and Space Administration, Langley Research Center - Available from NASA Center for AeroSpace Information
- Publish Date: 1999
- Publish Location: ➤ Hampton, Va - Springfield, VA - Hanover, MD
“F-16XL-2 supersonic laminar flow control flight test experiment” Subjects and Themes:
- Subjects: Computational fluid dynamics - Supersonic flow - Boundary layer control - Laminar flow - Design analysis
Edition Identifiers:
- The Open Library ID: OL18140131M - OL17595528M - OL15569345M - OL18296124M
- Online Computer Library Center (OCLC) ID: 44442105
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find F-16XL-2 supersonic laminar flow control flight test experiment at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
7Simulated-airline-service flight tests of laminar-flow control with perforated-surface suction system
By Dal V. Maddalon
“Simulated-airline-service flight tests of laminar-flow control with perforated-surface suction system” Metadata:
- Title: ➤ Simulated-airline-service flight tests of laminar-flow control with perforated-surface suction system
- Author: Dal V. Maddalon
- Language: English
- Number of Pages: Median: 38
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - Langley Research Center - For sale by the National Technical Information Service]
- Publish Date: 1990
- Publish Location: ➤ Hampton, Va - [Springfield, Va - [Washington, DC]
“Simulated-airline-service flight tests of laminar-flow control with perforated-surface suction system” Subjects and Themes:
- Subjects: Airplanes - Flight testing - Laminar flow - Boundary layer control
Edition Identifiers:
- The Open Library ID: OL15276863M - OL19380467M - OL17096532M - OL18029801M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Simulated-airline-service flight tests of laminar-flow control with perforated-surface suction system at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
8Three-dimensional boundary-layer program (BL3D) for swept subsonic or supersonic wings with application to laminar flow control
By Venkit Iyer
“Three-dimensional boundary-layer program (BL3D) for swept subsonic or supersonic wings with application to laminar flow control” Metadata:
- Title: ➤ Three-dimensional boundary-layer program (BL3D) for swept subsonic or supersonic wings with application to laminar flow control
- Author: Venkit Iyer
- Language: English
- Number of Pages: Median: 90
- Publisher: ➤ National Technical Information Service, distributor] - Langley Research Center - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1993
- Publish Location: ➤ Hampton, Va - [Springfield, Va - [Washington, DC]
“Three-dimensional boundary-layer program (BL3D) for swept subsonic or supersonic wings with application to laminar flow control” Subjects and Themes:
- Subjects: ➤ Boundary layer - Laminar flow - Three dimensional boundary layer - Boundary layer control - Swept wings
Edition Identifiers:
- The Open Library ID: OL19916683M - OL14699711M - OL15385040M - OL18064176M
Access and General Info:
- First Year Published: 1993
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Three-dimensional boundary-layer program (BL3D) for swept subsonic or supersonic wings with application to laminar flow control at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
9The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil
By Charles D. Harris
“The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil” Metadata:
- Title: ➤ The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil
- Author: Charles D. Harris
- Number of Pages: Median: 120
- Publisher: Langley Research Center
- Publish Date: 1988 - 1989 - 1992
- Publish Location: Hampton, Va
“The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL20898399M - OL19243776M - OL19379503M
Access and General Info:
- First Year Published: 1988
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
10Drag reduction by shock and boundary layer control
By E. Stanewsky

“Drag reduction by shock and boundary layer control” Metadata:
- Title: ➤ Drag reduction by shock and boundary layer control
- Author: E. Stanewsky
- Language: English
- Number of Pages: Median: 450
- Publisher: ➤ Springer-Verlag GmbH u. Co.KG - Springer
- Publish Date: 2002
- Publish Location: New York - Berlin
“Drag reduction by shock and boundary layer control” Subjects and Themes:
- Subjects: Research - Boundary layer control - Drag (aerodynamics) - Shock waves - Drag (Aerodynamics)
- Places: Europe
Edition Identifiers:
- The Open Library ID: OL22509332M - OL12775134M - OL20645031M
- Library of Congress Control Number (LCCN): 2002021689
- All ISBNs: 9783540433170 - 3540433171
Access and General Info:
- First Year Published: 2002
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Drag reduction by shock and boundary layer control at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
11Control of unsteady separated flow associated with the dynamic stall of airfoils
By Michael C. Wilder
“Control of unsteady separated flow associated with the dynamic stall of airfoils” Metadata:
- Title: ➤ Control of unsteady separated flow associated with the dynamic stall of airfoils
- Author: Michael C. Wilder
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor - MCAT Institute
- Publish Date: 1992 - 1994 - 1995
- Publish Location: ➤ Springfield, Va - [Washington, DC - Springfield, Va.? - San Jose, CA
“Control of unsteady separated flow associated with the dynamic stall of airfoils” Subjects and Themes:
- Subjects: ➤ Unsteady flow - Wind tunnel tests - Leading edges - Aerodynamic stalling - Boundary layer control - Unsteady flow (Aerodynamics) - Separated flow - Boundary layer separation - Reynolds number - Supercritical airfoils - Airfoil oscillations - Airfoil profiles - Airfoils - Mach number - Active control
Edition Identifiers:
- The Open Library ID: OL15365679M - OL15408283M - OL15415078M
Access and General Info:
- First Year Published: 1992
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Control of unsteady separated flow associated with the dynamic stall of airfoils at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
12Vortex/boundary-layer interactions, data report
By A. D. Cutler
“Vortex/boundary-layer interactions, data report” Metadata:
- Title: ➤ Vortex/boundary-layer interactions, data report
- Author: A. D. Cutler
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service - Imperial College of Science and Technology, Dept. of Technology - Imperial College of Science and Technology, Department of Aeronautics
- Publish Date: 1988
- Publish Location: [Springfield, Va - London
“Vortex/boundary-layer interactions, data report” Subjects and Themes:
- Subjects: Boundary layer control - Vortex-motion
Edition Identifiers:
- The Open Library ID: OL15276187M - OL18029870M - OL18029570M
Access and General Info:
- First Year Published: 1988
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Vortex/boundary-layer interactions, data report at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
13Supersonic laminar flow control research
By Ching F. Lo
“Supersonic laminar flow control research” Metadata:
- Title: ➤ Supersonic laminar flow control research
- Author: Ching F. Lo
- Language: English
- Publisher: ➤ Ames Research Center - National Aeronautics and Space Administration - University of Tennessee, Space Institute - National Technical Information Service, distributor
- Publish Date: 1995 - 1996
- Publish Location: ➤ Tullahoma, TN - [Springfield, Va - Moffett Field, CA - [Washington, DC - Springfield, Va
“Supersonic laminar flow control research” Subjects and Themes:
- Subjects: ➤ Boundary layer stability - Supersonic boundary layers - Boundary layer control - Supersonic flow - Laminar flow - Active control - Computational fluid dynamics - Control systems design - Boundary layer flow - Laminar boundary layer - Boundary layer transition - Wind tunnel nozzles - Stability - Temperature distribution - Wind tunnel tests - Laminar boundary - Wall temperature - Supersonic wind tunnels - Prediction analysis techniques - Nozzle design
Edition Identifiers:
- The Open Library ID: OL15543412M - OL15424662M - OL15506457M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Supersonic laminar flow control research at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
14Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction
By David S. Dolling
“Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction” Metadata:
- Title: ➤ Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction
- Author: David S. Dolling
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - Center for Aerodynamics Research, Dept. of Aerospace Engineering & Engineering Mechanics, University of Texas at Austin - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - Austin, Tex - [Washington, DC
“Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction” Subjects and Themes:
- Subjects: ➤ Turbulent boundary layer - Unsteady flow - Boundary layer separation - Aerodynamic loads - Corner flow - Vortex generators - Hypersonic boundary layer - Boundary layer control - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL18088579M - OL17803977M - OL15425915M
- Online Computer Library Center (OCLC) ID: 35454133
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
15Flow characteristics in boundary layer bleed slots with plenum
By A. Hamed
“Flow characteristics in boundary layer bleed slots with plenum” Metadata:
- Title: ➤ Flow characteristics in boundary layer bleed slots with plenum
- Author: A. Hamed
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - For sale by the National Technical Information Service
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Washington, D.C
“Flow characteristics in boundary layer bleed slots with plenum” Subjects and Themes:
- Subjects: ➤ Boundary layer control - Boundary layer flow - Flow characteristics - Oblique shock waves - Plenum chambers - Pressure gradients - Shock wave interaction - Slots - Supersonic flow - Turbulent boundary layer
Edition Identifiers:
- The Open Library ID: OL17793989M - OL15419025M
- Online Computer Library Center (OCLC) ID: 34757915
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Flow characteristics in boundary layer bleed slots with plenum at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
16Instability and transition of flow at, and near, an attachment-line
By A. Smith
“Instability and transition of flow at, and near, an attachment-line” Metadata:
- Title: ➤ Instability and transition of flow at, and near, an attachment-line
- Author: A. Smith
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996 - 1998
- Publish Location: ➤ Hampton, Va - [Washington, DC - [Springfield, Va - Springfield, Va
“Instability and transition of flow at, and near, an attachment-line” Subjects and Themes:
- Subjects: ➤ Boundary layer control - Boundary layer transition - Boundary layers - Control surfaces - Drag - Laminar boundary layer - Reynolds number - Stability - Transition flow - Turbulence - Wings
Edition Identifiers:
- The Open Library ID: OL15544664M - OL15547327M
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Instability and transition of flow at, and near, an attachment-line at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
17Control of flow instabilities and unsteady flows
By Gerd E. A. Meier

“Control of flow instabilities and unsteady flows” Metadata:
- Title: ➤ Control of flow instabilities and unsteady flows
- Author: Gerd E. A. Meier
- Language: English
- Number of Pages: Median: 325
- Publisher: Springer
- Publish Date: 1996 - 2002
- Publish Location: Wien - New York
“Control of flow instabilities and unsteady flows” Subjects and Themes:
- Subjects: Turbulence - Boundary layer control - Unsteady flow (Fluid dynamics) - Flow cytometry
Edition Identifiers:
- The Open Library ID: OL18096652M - OL12678259M
- Online Computer Library Center (OCLC) ID: 36311319
- All ISBNs: 9783211828076 - 3211828079
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Control of flow instabilities and unsteady flows at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
18EUROSHOCK
By Egon Stanewsky, Jean Delery, John Fulker and Wolfgang Geissler
“EUROSHOCK” Metadata:
- Title: EUROSHOCK
- Authors: Egon StanewskyJean DeleryJohn FulkerWolfgang Geissler
- Language: English
- Number of Pages: Median: 414
- Publisher: ➤ Vieweg - Friedrich Vieweg & Sohn Verlag
- Publish Date: 1997
- Publish Location: Braunschweig/Wiesbaden
“EUROSHOCK” Subjects and Themes:
- Subjects: ➤ Shock waves - Drag (Aerodynamics) - Boundary layer control - Transonic planes - Research - Wings - Design and construction
- Places: European Union countries
Edition Identifiers:
- The Open Library ID: OL12768781M - OL20954927M
- All ISBNs: 3528076569 - 9783528076566
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find EUROSHOCK at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
19IUTAM Symposium on Mechanics of Passive and Active Flow Control
By IUTAM Symposium on Mechanics of Passive and Active Flow Control (1998 Göttingen, Germany)

“IUTAM Symposium on Mechanics of Passive and Active Flow Control” Metadata:
- Title: ➤ IUTAM Symposium on Mechanics of Passive and Active Flow Control
- Author: ➤ IUTAM Symposium on Mechanics of Passive and Active Flow Control (1998 Göttingen, Germany)
- Language: English
- Number of Pages: Median: 387
- Publisher: Kluwer Academic - Springer
- Publish Date: 1999
- Publish Location: Dordrecht - Boston
“IUTAM Symposium on Mechanics of Passive and Active Flow Control” Subjects and Themes:
- Subjects: Congresses - Fluid dynamics - Boundary layer control
Edition Identifiers:
- The Open Library ID: OL9730152M - OL20643002M
- Online Computer Library Center (OCLC) ID: 41944759
- Library of Congress Control Number (LCCN): 99040883
- All ISBNs: 9780792359289 - 0792359283
First Setence:
"The boundary layers of practical interest are invariably turbulent, with drastically increased drag due to near-wall vortical coherent structures (CS)."
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find IUTAM Symposium on Mechanics of Passive and Active Flow Control at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
20Hybrid laminar flow control experiments in the NASA - Ames, 11-foot tunnel
By W. S. Saric
“Hybrid laminar flow control experiments in the NASA - Ames, 11-foot tunnel” Metadata:
- Title: ➤ Hybrid laminar flow control experiments in the NASA - Ames, 11-foot tunnel
- Author: W. S. Saric
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Washington, D.C
“Hybrid laminar flow control experiments in the NASA - Ames, 11-foot tunnel” Subjects and Themes:
- Subjects: ➤ Drag reduction - Surface roughness effects - Wind tunnel tests - Swept wings - Laminar boundary layer - Boundary layer control - Boundary layer transition - Turbulence effects
Edition Identifiers:
- The Open Library ID: OL15423184M - OL17796516M
- Online Computer Library Center (OCLC) ID: 35290580
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Hybrid laminar flow control experiments in the NASA - Ames, 11-foot tunnel at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
21Effect of nonzero surface admittance on receptivity and stability of compressible boundary layer
By Meelan Choudhari
“Effect of nonzero surface admittance on receptivity and stability of compressible boundary layer” Metadata:
- Title: ➤ Effect of nonzero surface admittance on receptivity and stability of compressible boundary layer
- Author: Meelan Choudhari
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1994
- Publish Location: [Springfield, Va - Hampton, Va
“Effect of nonzero surface admittance on receptivity and stability of compressible boundary layer” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - Boundary layer control - Boundary layer flow - Boundary layer stability - Compressible boundary layer - Suction - Two dimensional boundary layer
Edition Identifiers:
- The Open Library ID: OL17790197M - OL15403184M
- Online Computer Library Center (OCLC) ID: 32188843
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Effect of nonzero surface admittance on receptivity and stability of compressible boundary layer at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
22Numerical study of boundary-layer control in aerodynamics
By Tom I.-P Shih
“Numerical study of boundary-layer control in aerodynamics” Metadata:
- Title: ➤ Numerical study of boundary-layer control in aerodynamics
- Author: Tom I.-P Shih
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Numerical study of boundary-layer control in aerodynamics” Subjects and Themes:
- Subjects: Computational fluid dynamics - Aerodynamics - Boundary layer control - Boundary layer flow - Computer programs
Edition Identifiers:
- The Open Library ID: OL17837313M - OL15505971M
- Online Computer Library Center (OCLC) ID: 40190718
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Numerical study of boundary-layer control in aerodynamics at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
23Optimum suction distribution for transition control
By P. Balakumar
“Optimum suction distribution for transition control” Metadata:
- Title: ➤ Optimum suction distribution for transition control
- Author: P. Balakumar
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: Hampton, Va - [Springfield, Va
“Optimum suction distribution for transition control” Subjects and Themes:
- Subjects: ➤ Boundary layer control - Lagrange multipliers - Laminar flow - Newton-Raphson method - Optimization - Suction
Edition Identifiers:
- The Open Library ID: OL15505083M - OL17593320M
- Online Computer Library Center (OCLC) ID: 40173291
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Optimum suction distribution for transition control at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
24Buoyancy cross-flow effects on the boundary layer of a heated horizontal cylinder
By L. S Yao
“Buoyancy cross-flow effects on the boundary layer of a heated horizontal cylinder” Metadata:
- Title: ➤ Buoyancy cross-flow effects on the boundary layer of a heated horizontal cylinder
- Author: L. S Yao
- Language: English
- Number of Pages: Median: 15
- Publisher: Rand
- Publish Date: 1976
- Publish Location: Santa Monica
“Buoyancy cross-flow effects on the boundary layer of a heated horizontal cylinder” Subjects and Themes:
- Subjects: Boundary layer control
Edition Identifiers:
- The Open Library ID: OL15269262M - OL18095855M
Access and General Info:
- First Year Published: 1976
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Buoyancy cross-flow effects on the boundary layer of a heated horizontal cylinder at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
25Flowfield measurements in a slot-bled oblique shock wave and turbulent boundary-layer interaction
By D. O. Davis
“Flowfield measurements in a slot-bled oblique shock wave and turbulent boundary-layer interaction” Metadata:
- Title: ➤ Flowfield measurements in a slot-bled oblique shock wave and turbulent boundary-layer interaction
- Author: D. O. Davis
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Lewis Research Center
- Publish Date: 1998
- Publish Location: ➤ [Cleveland, Ohio] - Springfield, VA
“Flowfield measurements in a slot-bled oblique shock wave and turbulent boundary-layer interaction” Subjects and Themes:
- Subjects: ➤ Turbulent boundary layer - Flow measurement - Mass flow - Oblique shock waves - Boundary layer control - Boundary layer transition - Interactional aerodynamics - Slots - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL15541815M - OL17838705M
- Online Computer Library Center (OCLC) ID: 41323463
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Flowfield measurements in a slot-bled oblique shock wave and turbulent boundary-layer interaction at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
26Porous and microporous honeycomb composites as potential boundary-layer bleed materials
By D. O. Davis
“Porous and microporous honeycomb composites as potential boundary-layer bleed materials” Metadata:
- Title: ➤ Porous and microporous honeycomb composites as potential boundary-layer bleed materials
- Author: D. O. Davis
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, D.C
“Porous and microporous honeycomb composites as potential boundary-layer bleed materials” Subjects and Themes:
- Subjects: ➤ Boundary layer control - Honeycomb structures - Composite materials - Supersonic flow - Wind tunnel tests - Mach number
Edition Identifiers:
- The Open Library ID: OL15539875M - OL17838310M
- Online Computer Library Center (OCLC) ID: 40758884
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Porous and microporous honeycomb composites as potential boundary-layer bleed materials at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
27Investigation to optimize the passive shock wave/boundary layer control for supercritical airfoil drag reduction
By H. T. Nagamatsu
“Investigation to optimize the passive shock wave/boundary layer control for supercritical airfoil drag reduction” Metadata:
- Title: ➤ Investigation to optimize the passive shock wave/boundary layer control for supercritical airfoil drag reduction
- Author: H. T. Nagamatsu
- Language: English
- Publisher: NASA Langley Research Center
- Publish Date: 1983
- Publish Location: [Hampton, Va.?]
“Investigation to optimize the passive shock wave/boundary layer control for supercritical airfoil drag reduction” Subjects and Themes:
- Subjects: Boundary layer control - Aerofoils - Drag reduction - Supercritical wings - Shock waves
Edition Identifiers:
- The Open Library ID: OL16153613M - OL17635319M
- Online Computer Library Center (OCLC) ID: 173659340
Access and General Info:
- First Year Published: 1983
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Investigation to optimize the passive shock wave/boundary layer control for supercritical airfoil drag reduction at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
28On supersonic-inlet boundary-layer bleed flow
By G. J. Harloff
“On supersonic-inlet boundary-layer bleed flow” Metadata:
- Title: ➤ On supersonic-inlet boundary-layer bleed flow
- Author: G. J. Harloff
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“On supersonic-inlet boundary-layer bleed flow” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Bleeding - Mathematical models - Boundary conditions - Boundary layer flow - Boundary layer control - Compressible flow - Supersonic inlets
Edition Identifiers:
- The Open Library ID: OL15409168M - OL18078927M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find On supersonic-inlet boundary-layer bleed flow at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
29Vortex boundary-layer interactions, data report
By P. Bradshaw
“Vortex boundary-layer interactions, data report” Metadata:
- Title: ➤ Vortex boundary-layer interactions, data report
- Author: P. Bradshaw
- Language: English
- Publisher: ➤ Imperial College of Science and Technology, Department of Technology - For sale by the National Technical Information Service
- Publish Date: 1985
- Publish Location: [Springfield, Va - London
“Vortex boundary-layer interactions, data report” Subjects and Themes:
- Subjects: Boundary layer control - Vortex-motion
Edition Identifiers:
- The Open Library ID: OL15394472M - OL18069354M
Access and General Info:
- First Year Published: 1985
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Vortex boundary-layer interactions, data report at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
30Feasibility of generating an "artificial" burst in a turbulent boundary layer
By Mohamed Gad-el-Hak
“Feasibility of generating an "artificial" burst in a turbulent boundary layer” Metadata:
- Title: ➤ Feasibility of generating an "artificial" burst in a turbulent boundary layer
- Author: Mohamed Gad-el-Hak
- Number of Pages: Median: 90
- Publisher: Langley Research Center
- Publish Date: 1986 - 1989
- Publish Location: Hampton, Va
“Feasibility of generating an "artificial" burst in a turbulent boundary layer” Subjects and Themes:
- Subjects: ➤ Artificial burst - Boundary layer control - Drag reduction - Skin friction - Suction - Turbulent boundary layer
Edition Identifiers:
- The Open Library ID: OL18930332M - OL20983893M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Feasibility of generating an "artificial" burst in a turbulent boundary layer at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
31A description of the active and passive sidewall-boundary-layer removal systems of the 0.3-Meter Transonic Cryogenic Tunnel
By Charles B. Johnson
“A description of the active and passive sidewall-boundary-layer removal systems of the 0.3-Meter Transonic Cryogenic Tunnel” Metadata:
- Title: ➤ A description of the active and passive sidewall-boundary-layer removal systems of the 0.3-Meter Transonic Cryogenic Tunnel
- Author: Charles B. Johnson
- Language: English
- Number of Pages: Median: 18
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - Langley Research Center - For sale by the National Technical Information Service]
- Publish Date: 1986 - 1987
- Publish Location: ➤ Hampton, Va - [Springfield, Va - [Washington, DC]
“A description of the active and passive sidewall-boundary-layer removal systems of the 0.3-Meter Transonic Cryogenic Tunnel” Subjects and Themes:
- Subjects: Cryogenic wind tunnels - Boundary layer - Boundary layer control - Airfoils - High Reynolds number
Edition Identifiers:
- The Open Library ID: OL15286810M - OL20985413M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find A description of the active and passive sidewall-boundary-layer removal systems of the 0.3-Meter Transonic Cryogenic Tunnel at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
32The use of air injection to prevent separation of the turbulent boundary layer in supersonic flow
By D. J. Peake
“The use of air injection to prevent separation of the turbulent boundary layer in supersonic flow” Metadata:
- Title: ➤ The use of air injection to prevent separation of the turbulent boundary layer in supersonic flow
- Author: D. J. Peake
- Language: English
- Number of Pages: Median: 30
- Publisher: H.M.S.O.
- Publish Date: 1967
- Publish Location: London
“The use of air injection to prevent separation of the turbulent boundary layer in supersonic flow” Subjects and Themes:
- Subjects: Air jets - Boundary layer control - Supersonic Aerodynamics - Turbulence
Edition Identifiers:
- The Open Library ID: OL5570692M
- Library of Congress Control Number (LCCN): 67078700
Access and General Info:
- First Year Published: 1967
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find The use of air injection to prevent separation of the turbulent boundary layer in supersonic flow at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
33Low-speed wind-tunnel tests on a delta-wing aircraft model (S.R. 177) with blowing over the trailing-edge flaps and ailerons
By S. F. J. Butler
“Low-speed wind-tunnel tests on a delta-wing aircraft model (S.R. 177) with blowing over the trailing-edge flaps and ailerons” Metadata:
- Title: ➤ Low-speed wind-tunnel tests on a delta-wing aircraft model (S.R. 177) with blowing over the trailing-edge flaps and ailerons
- Author: S. F. J. Butler
- Language: English
- Number of Pages: Median: 32
- Publisher: H.M.S.O.
- Publish Date: 1966
- Publish Location: London
“Low-speed wind-tunnel tests on a delta-wing aircraft model (S.R. 177) with blowing over the trailing-edge flaps and ailerons” Subjects and Themes:
- Subjects: Aerodynamics - Airplanes - Boundary layer control - Triangular Wings
Edition Identifiers:
- The Open Library ID: OL6019028M
- Library of Congress Control Number (LCCN): 66078164
Access and General Info:
- First Year Published: 1966
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Low-speed wind-tunnel tests on a delta-wing aircraft model (S.R. 177) with blowing over the trailing-edge flaps and ailerons at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
34Investigation to optimize the passive shock wave/boundary layer control for supercritical airfoil drag reduction
By Henry T. Nagamatsu
“Investigation to optimize the passive shock wave/boundary layer control for supercritical airfoil drag reduction” Metadata:
- Title: ➤ Investigation to optimize the passive shock wave/boundary layer control for supercritical airfoil drag reduction
- Author: Henry T. Nagamatsu
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1984
- Publish Location: [Hampton, Va.?
“Investigation to optimize the passive shock wave/boundary layer control for supercritical airfoil drag reduction” Subjects and Themes:
- Subjects: Aerofoils - Boundary layer control
Edition Identifiers:
- The Open Library ID: OL15396095M
Access and General Info:
- First Year Published: 1984
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Investigation to optimize the passive shock wave/boundary layer control for supercritical airfoil drag reduction at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
35Boundary layer and flow control
By Gustav Victor Lachmann
“Boundary layer and flow control” Metadata:
- Title: ➤ Boundary layer and flow control
- Author: Gustav Victor Lachmann
- Language: English
- Number of Pages: Median: 1360
- Publisher: Pergamon Press
- Publish Date: 1961
- Publish Location: New York
“Boundary layer and flow control” Subjects and Themes:
- Subjects: Boundary layer control - Boundary layer
Edition Identifiers:
- The Open Library ID: OL14125414M
- Online Computer Library Center (OCLC) ID: 4312920
- Library of Congress Control Number (LCCN): 60009645
Access and General Info:
- First Year Published: 1961
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Boundary layer and flow control at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
36Performance of the active sidewall boundary-layer removal system for the Langley 0.3-meter transonic cryogenic tunnel
By Balakrishna, S.
“Performance of the active sidewall boundary-layer removal system for the Langley 0.3-meter transonic cryogenic tunnel” Metadata:
- Title: ➤ Performance of the active sidewall boundary-layer removal system for the Langley 0.3-meter transonic cryogenic tunnel
- Author: Balakrishna, S.
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1989
- Publish Location: [Springfield, Va - Hampton, Va
“Performance of the active sidewall boundary-layer removal system for the Langley 0.3-meter transonic cryogenic tunnel” Subjects and Themes:
- Subjects: ➤ Boundary layer control - Compressors - Cryogenic wind tunnels - Mass flow - Removal - Transonic wind tunnels - Wind tunnel walls
Edition Identifiers:
- The Open Library ID: OL15407608M
Access and General Info:
- First Year Published: 1989
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Performance of the active sidewall boundary-layer removal system for the Langley 0.3-meter transonic cryogenic tunnel at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
37Controlling the separation of laminar boundary layers in water
By Jerome Aroesty
“Controlling the separation of laminar boundary layers in water” Metadata:
- Title: ➤ Controlling the separation of laminar boundary layers in water
- Author: Jerome Aroesty
- Language: English
- Number of Pages: Median: 29
- Publisher: Rand
- Publish Date: 1975
- Publish Location: Santa Monica
“Controlling the separation of laminar boundary layers in water” Subjects and Themes:
- Subjects: Boundary layer control - Laminar flow
Edition Identifiers:
- The Open Library ID: OL15269077M
Access and General Info:
- First Year Published: 1975
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Controlling the separation of laminar boundary layers in water at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
38Boundary layer flow control with a One Atmosphere Uniform Glow Discharge Surface Plasma
By J. Reece Roth
“Boundary layer flow control with a One Atmosphere Uniform Glow Discharge Surface Plasma” Metadata:
- Title: ➤ Boundary layer flow control with a One Atmosphere Uniform Glow Discharge Surface Plasma
- Author: J. Reece Roth
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - American Institute of Aeronautics and Astronautics - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: ➤ Springfield, Va - [Washington, DC - Reston, Va
“Boundary layer flow control with a One Atmosphere Uniform Glow Discharge Surface Plasma” Subjects and Themes:
- Subjects: ➤ Boundary layer control - Plasmas (Physics) - Wind tunnel tests - Boundary layer flow - Data acquisition - Glow discharges
Edition Identifiers:
- The Open Library ID: OL15547651M
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Boundary layer flow control with a One Atmosphere Uniform Glow Discharge Surface Plasma at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
39Investigations into increasing the lift of wings by boundary layer control through blowing
By Thomas, Fred
“Investigations into increasing the lift of wings by boundary layer control through blowing” Metadata:
- Title: ➤ Investigations into increasing the lift of wings by boundary layer control through blowing
- Author: Thomas, Fred
- Language: English
- Number of Pages: Median: 45
- Publisher: Ministry of Technology
- Publish Date: 1967
- Publish Location: Farnborough [Eng.]
“Investigations into increasing the lift of wings by boundary layer control through blowing” Subjects and Themes:
- Subjects: Boundary layer control - Lift (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL4370835M
- Library of Congress Control Number (LCCN): 78555017
Access and General Info:
- First Year Published: 1967
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Investigations into increasing the lift of wings by boundary layer control through blowing at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
40Forum on Unsteady Flow Separation
By Forum on Unsteady Flow Separation (1987 Cincinnati, Ohio)
“Forum on Unsteady Flow Separation” Metadata:
- Title: ➤ Forum on Unsteady Flow Separation
- Author: ➤ Forum on Unsteady Flow Separation (1987 Cincinnati, Ohio)
- Language: English
- Number of Pages: Median: 249
- Publisher: ➤ American Society of Mechanical Engineers
- Publish Date: 1987
- Publish Location: ➤ New York, N.Y. (345 E. 47th St., New York 10017)
“Forum on Unsteady Flow Separation” Subjects and Themes:
- Subjects: Boundary layer control - Congresses - Unsteady flow (Fluid dynamics)
Edition Identifiers:
- The Open Library ID: OL2413493M
- Library of Congress Control Number (LCCN): 87071410
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Forum on Unsteady Flow Separation at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
41Recent development in flow separation
By Paul K. Chang
“Recent development in flow separation” Metadata:
- Title: ➤ Recent development in flow separation
- Author: Paul K. Chang
- Language: English
- Number of Pages: Median: 353
- Publisher: Pang Han Pub. Co.
- Publish Date: 1985
- Publish Location: Seoul, Korea
“Recent development in flow separation” Subjects and Themes:
- Subjects: Boundary layer control - Fluid dynamics
Edition Identifiers:
- The Open Library ID: OL3193283M
- Online Computer Library Center (OCLC) ID: 13185640
- Library of Congress Control Number (LCCN): 83072431
- All ISBNs: 0961241063 - 9780961241063
Access and General Info:
- First Year Published: 1985
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Recent development in flow separation at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
42Modifications to the Langley 8-foot transonic pressure tunnel for the laminar flow control experiment
By Charles D. Harris
“Modifications to the Langley 8-foot transonic pressure tunnel for the laminar flow control experiment” Metadata:
- Title: ➤ Modifications to the Langley 8-foot transonic pressure tunnel for the laminar flow control experiment
- Author: Charles D. Harris
- Number of Pages: Median: 120
- Publisher: Langley Research Center
- Publish Date: 1988
- Publish Location: Hampton, Va
“Modifications to the Langley 8-foot transonic pressure tunnel for the laminar flow control experiment” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL20898422M
Access and General Info:
- First Year Published: 1988
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Modifications to the Langley 8-foot transonic pressure tunnel for the laminar flow control experiment at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
43Experimental investigation of airfoil boundary-layer receptivity and a method for the characterization of the relevant free-stream disturbances
By Stefan Herr
“Experimental investigation of airfoil boundary-layer receptivity and a method for the characterization of the relevant free-stream disturbances” Metadata:
- Title: ➤ Experimental investigation of airfoil boundary-layer receptivity and a method for the characterization of the relevant free-stream disturbances
- Author: Stefan Herr
- Language: ger
- Number of Pages: Median: 121
- Publisher: Verlag Dr. Hut
- Publish Date: 2004
- Publish Location: München
“Experimental investigation of airfoil boundary-layer receptivity and a method for the characterization of the relevant free-stream disturbances” Subjects and Themes:
- Subjects: Aerodynamics - Boundary layer control - Aerofoils
Edition Identifiers:
- The Open Library ID: OL24486577M
- Library of Congress Control Number (LCCN): 2008395594
- All ISBNs: 9783899630527 - 3899630521
Access and General Info:
- First Year Published: 2004
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Experimental investigation of airfoil boundary-layer receptivity and a method for the characterization of the relevant free-stream disturbances at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
44Analysis and evaluation of an integrated laminar flow control propulsion system
By Theodore G. Keith
“Analysis and evaluation of an integrated laminar flow control propulsion system” Metadata:
- Title: ➤ Analysis and evaluation of an integrated laminar flow control propulsion system
- Author: Theodore G. Keith
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1993
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Analysis and evaluation of an integrated laminar flow control propulsion system” Subjects and Themes:
- Subjects: ➤ Turbulent flow - Skin friction - Transport aircraft - Drag reduction - Friction reduction - Friction drag - Laminar boundary layer - Aerodynamic drag - Boundary layer control - Friction factor - Suction
Edition Identifiers:
- The Open Library ID: OL17683011M
Access and General Info:
- First Year Published: 1993
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Analysis and evaluation of an integrated laminar flow control propulsion system at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
45Effect of suction on controlling the secondary instability of boundary layers
By Nabil M. El-Hady
“Effect of suction on controlling the secondary instability of boundary layers” Metadata:
- Title: ➤ Effect of suction on controlling the secondary instability of boundary layers
- Author: Nabil M. El-Hady
- Language: English
- Number of Pages: Median: 33
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - For sale by the National Technical Information Service]
- Publish Date: 1990
- Publish Location: ➤ Washington, D.C - [Springfield, Va
“Effect of suction on controlling the secondary instability of boundary layers” Subjects and Themes:
- Subjects: ➤ Stability - Secondary flow - Boundary layer control - Boundary layer stability - Suction - Boundary layer - Laminar flow
Edition Identifiers:
- The Open Library ID: OL16131162M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Effect of suction on controlling the secondary instability of boundary layers at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
46Parametric study on laminar flow for finite wings at supersonic speeds
By Joseph Avila Garcia
“Parametric study on laminar flow for finite wings at supersonic speeds” Metadata:
- Title: ➤ Parametric study on laminar flow for finite wings at supersonic speeds
- Author: Joseph Avila Garcia
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Parametric study on laminar flow for finite wings at supersonic speeds” Subjects and Themes:
- Subjects: ➤ Laminar boundary layer - Boundary layer control - Boundary layer stability - Supersonic speed - Wings - Laminar flow
Edition Identifiers:
- The Open Library ID: OL15412001M
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Parametric study on laminar flow for finite wings at supersonic speeds at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
47Effect of aspect ratio on sidewall boundary-layer influence in two-dimensional airfoil testing
By A. V Murthy
“Effect of aspect ratio on sidewall boundary-layer influence in two-dimensional airfoil testing” Metadata:
- Title: ➤ Effect of aspect ratio on sidewall boundary-layer influence in two-dimensional airfoil testing
- Author: A. V Murthy
- Language: English
- Number of Pages: Median: 28
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - National Technical Information Service, distributor]
- Publish Date: 1986
- Publish Location: ➤ [Springfield, Va - Washington, D.C
“Effect of aspect ratio on sidewall boundary-layer influence in two-dimensional airfoil testing” Subjects and Themes:
- Subjects: Wind tunnels - Boundary layer control - Flow visualization
Edition Identifiers:
- The Open Library ID: OL14984760M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Effect of aspect ratio on sidewall boundary-layer influence in two-dimensional airfoil testing at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
48Experiments to verify nonparallel stability theory at Virginia Polytechnic Institute and State University, Blacksburg, Virginia
By W. S. Saric
“Experiments to verify nonparallel stability theory at Virginia Polytechnic Institute and State University, Blacksburg, Virginia” Metadata:
- Title: ➤ Experiments to verify nonparallel stability theory at Virginia Polytechnic Institute and State University, Blacksburg, Virginia
- Author: W. S. Saric
- Language: English
- Publisher: ➤ Dept. of Mechanical and Aerospace Engineering, Arizona State University - National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1988
- Publish Location: ➤ Springfield, Va - Tempe, Ariz - [Washington, DC
“Experiments to verify nonparallel stability theory at Virginia Polytechnic Institute and State University, Blacksburg, Virginia” Subjects and Themes:
- Subjects: ➤ Blowing - Laminar boundary layer - Perforated plates - Wind tunnel tests - Boundary layer stability - Boundary layer control - Boundary layer transition - Reynolds number suction
Edition Identifiers:
- The Open Library ID: OL15408168M
Access and General Info:
- First Year Published: 1988
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Experiments to verify nonparallel stability theory at Virginia Polytechnic Institute and State University, Blacksburg, Virginia at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
49Submarine design optimization using boundary layer control
By Christopher L. Warren

“Submarine design optimization using boundary layer control” Metadata:
- Title: ➤ Submarine design optimization using boundary layer control
- Author: Christopher L. Warren
- Language: English
- Number of Pages: Median: 67
- Publisher: ➤ Available from National Technical Information Service
- Publish Date: 1997
- Publish Location: Springfield, Va
“Submarine design optimization using boundary layer control” Subjects and Themes:
- Subjects: SUBMARINE HULLS - BOUNDARY LAYER CONTROL - HULLS (STRUCTURES)
Edition Identifiers:
- The Open Library ID: OL25312172M
- Online Computer Library Center (OCLC) ID: 640482043
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: Yes
- Is The Book Public: Yes
- Access Status: Public
Online Access
Online Borrowing:
- Borrowing from Open Library: Borrowing link
- Borrowing from Archive.org: Borrowing link
Online Marketplaces
Find Submarine design optimization using boundary layer control at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
50Uniform stabilization of the Euler-Bernoulli equation with active Dirichlet and non-active Neumann boundary feedback controls
By Jerry Bartolomeo

“Uniform stabilization of the Euler-Bernoulli equation with active Dirichlet and non-active Neumann boundary feedback controls” Metadata:
- Title: ➤ Uniform stabilization of the Euler-Bernoulli equation with active Dirichlet and non-active Neumann boundary feedback controls
- Author: Jerry Bartolomeo
- Language: English
- Number of Pages: Median: 47
- Publish Date: 1988
“Uniform stabilization of the Euler-Bernoulli equation with active Dirichlet and non-active Neumann boundary feedback controls” Subjects and Themes:
- Subjects: Bernoulli polynomials - Hilbert space - Boundary layer control - Partial Differential equations
Edition Identifiers:
- The Open Library ID: OL24440926M
- Online Computer Library Center (OCLC) ID: 19976728
Access and General Info:
- First Year Published: 1988
- Is Full Text Available: Yes
- Is The Book Public: Yes
- Access Status: Public
Online Access
Online Borrowing:
- Borrowing from Open Library: Borrowing link
- Borrowing from Archive.org: Borrowing link
Online Marketplaces
Find Uniform stabilization of the Euler-Bernoulli equation with active Dirichlet and non-active Neumann boundary feedback controls at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.