Explore: Drag (aerodynamics)
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AI-Generated Overview About “drag-%28aerodynamics%29”:
Books Results
Source: The Open Library
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1Shape and flow
By Ascher H. Shapiro

“Shape and flow” Metadata:
- Title: Shape and flow
- Author: Ascher H. Shapiro
- Language: English
- Number of Pages: Median: 186
- Publisher: ➤ Anchor Books - Heinemann - Anchor Books/ Doubleday
- Publish Date: 1961 - 1964
- Publish Location: Garden City, N.Y - London
“Shape and flow” Subjects and Themes:
- Subjects: ➤ Drag (Aerodynamics) - Fluid dynamics - Frictional resistance (Hydrodynamics)
Edition Identifiers:
- The Open Library ID: OL19729508M - OL5825300M - OL16742775M - OL43140701M
- Online Computer Library Center (OCLC) ID: 239104
- Library of Congress Control Number (LCCN): 61012581
- All ISBNs: 0435550322 - 9780435550325
Author's Alternative Names:
"A. H. Shapiro", "Shapiro, Ascher, H." and "Ascher Herman Shapiro"Access and General Info:
- First Year Published: 1961
- Is Full Text Available: Yes
- Is The Book Public: No
- Access Status: Borrowable
Online Access
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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.
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- Borrowing from Archive.org: Borrowing link
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2Theory of satellite orbits in an atmosphere
By Desmond King-Hele

“Theory of satellite orbits in an atmosphere” Metadata:
- Title: ➤ Theory of satellite orbits in an atmosphere
- Author: Desmond King-Hele
- Language: English
- Number of Pages: Median: 165
- Publisher: Butterworths
- Publish Date: 1964
- Publish Location: London
“Theory of satellite orbits in an atmosphere” Subjects and Themes:
- Subjects: Artificial satellites - Upper Atmosphere - Orbits - Drag (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL5906431M
- Online Computer Library Center (OCLC) ID: 2312579
- Library of Congress Control Number (LCCN): 64005703
Access and General Info:
- First Year Published: 1964
- Is Full Text Available: Yes
- Is The Book Public: No
- Access Status: Borrowable
Online Access
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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.
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- Borrowing from Archive.org: Borrowing link
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3Viscous Flow Drag Reduction Paas72 (Progress in astronautics and aeronautics)
By Gary R. Hough

“Viscous Flow Drag Reduction Paas72 (Progress in astronautics and aeronautics)” Metadata:
- Title: ➤ Viscous Flow Drag Reduction Paas72 (Progress in astronautics and aeronautics)
- Author: Gary R. Hough
- Language: English
- Number of Pages: Median: 453
- Publisher: ➤ American Institute of Aeronautics and Astronautics - Amer Inst of Aeronautics &
- Publish Date: 1980
- Publish Location: New York
“Viscous Flow Drag Reduction Paas72 (Progress in astronautics and aeronautics)” Subjects and Themes:
- Subjects: ➤ Turbulent boundary layer - Drag (Aerodynamics) - Frictional resistance (Hydrodynamics) - Skin friction (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL4112639M - OL8336236M
- Online Computer Library Center (OCLC) ID: 7168961
- Library of Congress Control Number (LCCN): 80027715
- All ISBNs: 9780915928446 - 0915928442
Access and General Info:
- First Year Published: 1980
- Is Full Text Available: Yes
- Is The Book Public: No
- Access Status: Borrowable
Online Access
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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.
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- Borrowing from Archive.org: Borrowing link
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4Fluid-dynamic drag
By Sighard F. Hoerner

“Fluid-dynamic drag” Metadata:
- Title: Fluid-dynamic drag
- Author: Sighard F. Hoerner
- Language: English
- Publisher: ➤ Hoerner Fluid Dynamics - S.F. Hoerner
- Publish Date: 1958 - 1965 - 1992
- Publish Location: ➤ Midland Park, N.J.] - [Midland Park, N.J.] - Vancouver, WA - Midland Park, N.J
“Fluid-dynamic drag” Subjects and Themes:
- Subjects: Drag (Aerodynamics) - Ship resistance
Edition Identifiers:
- The Open Library ID: ➤ OL17462293M - OL6226523M - OL5916747M - OL49927249M - OL17463662M - OL16529069M
- Online Computer Library Center (OCLC) ID: 40593334 - 518197 - 1905249
- Library of Congress Control Number (LCCN): 64019666 - 57013009
Access and General Info:
- First Year Published: 1958
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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5Optimal pitch thrust-vector angle and benefits for all flight regimes
By Glenn B. Gilyard
“Optimal pitch thrust-vector angle and benefits for all flight regimes” Metadata:
- Title: ➤ Optimal pitch thrust-vector angle and benefits for all flight regimes
- Author: Glenn B. Gilyard
- Language: English
- Number of Pages: Median: 22
- Publisher: ➤ National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor
- Publish Date: 2000
- Publish Location: ➤ [Springfield, Va - Edwards, Calif
“Optimal pitch thrust-vector angle and benefits for all flight regimes” Subjects and Themes:
- Subjects: ➤ Airplanes - Angles (Geometry) - Automatic flight control - Control surfaces - Drag (Aerodynamics) - Flight testing - Handling characteristics - Lift (Aerodynamics) - Motors - Pitch (Inclination) - Thrust - Thrust vector control
Edition Identifiers:
- The Open Library ID: ➤ OL17704162M - OL20639635M - OL17596831M - OL18318816M - OL18302177M - OL18140962M
- Online Computer Library Center (OCLC) ID: 45009655
Access and General Info:
- First Year Published: 2000
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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6The 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
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7In-flight transport performance optimization
By Glenn B. Gilyard
“In-flight transport performance optimization” Metadata:
- Title: ➤ In-flight transport performance optimization
- Author: Glenn B. Gilyard
- Language: English
- Number of Pages: Median: 15
- Publisher: ➤ National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Springfield, Va - Edwards, Calif
“In-flight transport performance optimization” Subjects and Themes:
- Subjects: ➤ Ailerons - Airplanes - Transport vehicles - Real time operation - Cambered wings - Wing loading - Flight tests - Optimization - Aerodynamic drag - L-1011 aircraft - Handling characteristics - Jet transports - Flight testing - Wings - Drag (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL18118712M - OL17125500M - OL17572312M - OL17697192M - OL18889777M
- Online Computer Library Center (OCLC) ID: 39824781
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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8Viscous Drag Reduction
By C. Sinclair Wells
“Viscous Drag Reduction” Metadata:
- Title: Viscous Drag Reduction
- Author: C. Sinclair Wells
- Language: English
- Publisher: Plenum Press - Springer
- Publish Date: 1969 - 2013
“Viscous Drag Reduction” Subjects and Themes:
- Subjects: Drag (aerodynamics) - Fluid mechanics
Edition Identifiers:
- The Open Library ID: OL37420048M - OL43192813M - OL45751950M - OL37182815M
- All ISBNs: 9781489955814 - 148995581X - 1489955798 - 9781489955791
Access and General Info:
- First Year Published: 1969
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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9Wave drag and high-speed performance of supersonic STOVL fighter configurations
By D. A. Durston
“Wave drag and high-speed performance of supersonic STOVL fighter configurations” Metadata:
- Title: ➤ Wave drag and high-speed performance of supersonic STOVL fighter configurations
- Author: D. A. Durston
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1988
- Publish Location: Moffett Field, Calif
“Wave drag and high-speed performance of supersonic STOVL fighter configurations” Subjects and Themes:
- Subjects: Aerodynamics - Drag (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL15275844M - OL14664183M - OL18029449M - OL17096239M
Access and General Info:
- First Year Published: 1988
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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10Methods for estimating drag polars of subsonic airplanes
By Jan Roskam
“Methods for estimating drag polars of subsonic airplanes” Metadata:
- Title: ➤ Methods for estimating drag polars of subsonic airplanes
- Author: Jan Roskam
- Language: English
- Publish Date: 1971
- Publish Location: [Lawrence? Kan
“Methods for estimating drag polars of subsonic airplanes” Subjects and Themes:
- Subjects: Drag (Aerodynamics) - Tables
Edition Identifiers:
- The Open Library ID: OL5470293M
- Library of Congress Control Number (LCCN): 73173351
Access and General Info:
- First Year Published: 1971
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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11Drag 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
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12Effects of wing leading-edge flap deflections on subsonic longitudinal aerodynamic characteristics of a wing-fuselage configuration with a 44 ̊swept wing
By William P. Henderson
“Effects of wing leading-edge flap deflections on subsonic longitudinal aerodynamic characteristics of a wing-fuselage configuration with a 44 ̊swept wing” Metadata:
- Title: ➤ Effects of wing leading-edge flap deflections on subsonic longitudinal aerodynamic characteristics of a wing-fuselage configuration with a 44 ̊swept wing
- Author: William P. Henderson
- Language: English
- Number of Pages: Median: 35
- Publisher: ➤ for sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Office
- Publish Date: 1978
- Publish Location: [Washington] - Springfield, Va
“Effects of wing leading-edge flap deflections on subsonic longitudinal aerodynamic characteristics of a wing-fuselage configuration with a 44 ̊swept wing” Subjects and Themes:
- Subjects: Leading edges (Aerodynamics) - Drag (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL17538795M - OL18014728M - OL15231154M
Access and General Info:
- First Year Published: 1978
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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13Drag of two-dimensional small-amplitude symmetric and asymmetric wavy walls in turbulent boundary layers
By John C. Lin
“Drag of two-dimensional small-amplitude symmetric and asymmetric wavy walls in turbulent boundary layers” Metadata:
- Title: ➤ Drag of two-dimensional small-amplitude symmetric and asymmetric wavy walls in turbulent boundary layers
- Author: John C. Lin
- Language: English
- Number of Pages: Median: 162
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
- Publish Date: 1984
- Publish Location: ➤ [Springfield, Va - Washington, D.C
“Drag of two-dimensional small-amplitude symmetric and asymmetric wavy walls in turbulent boundary layers” Subjects and Themes:
- Subjects: Aerodynamics - Turbulent boundary layer - Drag (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL15312646M - OL17556403M - OL18039002M
Access and General Info:
- First Year Published: 1984
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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14Full-scale wind-tunnel investigation of the advanced technology light twin-engine airplane (ATLIT)
By James L. Hassell
“Full-scale wind-tunnel investigation of the advanced technology light twin-engine airplane (ATLIT)” Metadata:
- Title: ➤ Full-scale wind-tunnel investigation of the advanced technology light twin-engine airplane (ATLIT)
- Author: James L. Hassell
- Language: English
- Number of Pages: Median: 209
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Office
- Publish Date: 1980
- Publish Location: ➤ Washington, D.C - [Springfield, Va
“Full-scale wind-tunnel investigation of the advanced technology light twin-engine airplane (ATLIT)” Subjects and Themes:
- Subjects: ➤ Airplanes - Handling characteristics - Control systems - Performance - Stability of airplanes - Drag (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL17549943M - OL15263215M - OL18024175M
Access and General Info:
- First Year Published: 1980
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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15Flight-measured pressure characteristics of aft-facing steps in high Reynolds number flow at Mach numbers of 2.20, 2.50, and 2.80 and comparison with other data
By Sheryll Goecke Powers
“Flight-measured pressure characteristics of aft-facing steps in high Reynolds number flow at Mach numbers of 2.20, 2.50, and 2.80 and comparison with other data” Metadata:
- Title: ➤ Flight-measured pressure characteristics of aft-facing steps in high Reynolds number flow at Mach numbers of 2.20, 2.50, and 2.80 and comparison with other data
- Author: Sheryll Goecke Powers
- Language: English
- Number of Pages: Median: 35
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Office - for sale by the National Technical Information Office
- Publish Date: 1978
- Publish Location: Springfield, Va - [Washington]
“Flight-measured pressure characteristics of aft-facing steps in high Reynolds number flow at Mach numbers of 2.20, 2.50, and 2.80 and comparison with other data” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL15224938M - OL18013765M - OL17118190M
Access and General Info:
- First Year Published: 1978
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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16Flight and wind-tunnel measurements showing base drag reduction provided by a trailing disk for high Reynolds number turbulent flow for subsonic and transonic Mach numbers
By Sheryll Goecke Powers
“Flight and wind-tunnel measurements showing base drag reduction provided by a trailing disk for high Reynolds number turbulent flow for subsonic and transonic Mach numbers” Metadata:
- Title: ➤ Flight and wind-tunnel measurements showing base drag reduction provided by a trailing disk for high Reynolds number turbulent flow for subsonic and transonic Mach numbers
- Author: Sheryll Goecke Powers
- Language: English
- Number of Pages: Median: 139
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch - Dryden Flight Research Facility
- Publish Date: 1986 - 1988
- Publish Location: ➤ Edwards, Cal - [Springfield, Va - [Washington, DC]
“Flight and wind-tunnel measurements showing base drag reduction provided by a trailing disk for high Reynolds number turbulent flow for subsonic and transonic Mach numbers” Subjects and Themes:
- Subjects: ➤ Turbulent flow - Blunt bodies - Drag reduction - Trapped vortexes - Bodies of revolution - Mach number - Drag (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL15276247M - OL20985601M - OL18029606M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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17The natural flow wing-design concept
By Richard M. Wood
“The natural flow wing-design concept” Metadata:
- Title: ➤ The natural flow wing-design concept
- Author: Richard M. Wood
- Language: English
- Number of Pages: Median: 40
- Publisher: ➤ Langley Research Center - For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1992
- Publish Location: ➤ Hampton, Va - [Springfield, Va - [Washington, DC]
“The natural flow wing-design concept” Subjects and Themes:
- Subjects: ➤ Aerodynamics, Supersonic - Airplanes - Design and construction - Drag (Aerodynamics) - Supersonic Aerodynamics - Triangular Wings - Wings - Wings, Triangular
Edition Identifiers:
- The Open Library ID: OL19244112M - OL18053639M - OL15361632M
Access and General Info:
- First Year Published: 1992
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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18A theory of gas-surface interactions at satellite velocities
By D. P. Jackson
“A theory of gas-surface interactions at satellite velocities” Metadata:
- Title: ➤ A theory of gas-surface interactions at satellite velocities
- Author: D. P. Jackson
- Language: English
- Number of Pages: Median: 76
- Publisher: ➤ Institute for Aerospace Studies - [Institute for Aerospace Studies] - Institute for Aerospace Studies, University of Toronto]
- Publish Date: 1968
- Publish Location: [Toronto - [Downsview, Ont.]
“A theory of gas-surface interactions at satellite velocities” Subjects and Themes:
- Subjects: Artificial satellites - Drag (Aerodynamics) - Gas-surface interactions - Hypersonic Aerodynamics
Edition Identifiers:
- The Open Library ID: OL5011791M - OL19001626M - OL20986497M
- Library of Congress Control Number (LCCN): 76571665
Access and General Info:
- First Year Published: 1968
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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19Aerodynamic drag
By Sighard F. Hoerner
“Aerodynamic drag” Metadata:
- Title: Aerodynamic drag
- Author: Sighard F. Hoerner
- Language: English
- Number of Pages: Median: 259
- Publish Date: 1951
- Publish Location: ➤ [Midland Park, N.J.] - [Midland Park? N. J.]
“Aerodynamic drag” Subjects and Themes:
- Subjects: Drag (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL16529071M - OL14137055M
- Online Computer Library Center (OCLC) ID: 2460450
- Library of Congress Control Number (LCCN): 52019541
Access and General Info:
- First Year Published: 1951
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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20Summary of studies to reduce wing-mounted propfan installation drag on an M=0.8 transport
By Ronald C. Smith
“Summary of studies to reduce wing-mounted propfan installation drag on an M=0.8 transport” Metadata:
- Title: ➤ Summary of studies to reduce wing-mounted propfan installation drag on an M=0.8 transport
- Author: Ronald C. Smith
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1987
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va
“Summary of studies to reduce wing-mounted propfan installation drag on an M=0.8 transport” Subjects and Themes:
- Subjects: Drag (Aerodynamics) - Transport planes
Edition Identifiers:
- The Open Library ID: OL17658577M - OL14663126M
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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21EUROSHOCK
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
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22On the use of external burning to reduce aerospace vehicle transonic drag
By Charles J. Trefny
“On the use of external burning to reduce aerospace vehicle transonic drag” Metadata:
- Title: ➤ On the use of external burning to reduce aerospace vehicle transonic drag
- Author: Charles J. Trefny
- Language: English
- Number of Pages: Median: 14
- Publisher: ➤ For sale by the National Technical Information Service - NASA
- Publish Date: 1990
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va
“On the use of external burning to reduce aerospace vehicle transonic drag” Subjects and Themes:
- Subjects: ➤ Aerodynamics - Space vehicles - Drag (Aerodynamics) - Combustion - Turbojet engines - Drag reduction - Flame stability - Aerospace vehicles - Reaction kinetics - Aerodynamic drag - Hydrogen
Edition Identifiers:
- The Open Library ID: OL17630522M - OL16135223M
- Online Computer Library Center (OCLC) ID: 30712306
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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23Identification of intgrated airframe
By Gerard S. Schkolnik
“Identification of intgrated airframe” Metadata:
- Title: ➤ Identification of intgrated airframe
- Author: Gerard S. Schkolnik
- Language: English
- Publisher: ➤ National Technical Information Service, distributor] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1993
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Identification of intgrated airframe” Subjects and Themes:
- Subjects: Drag (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL14705233M - OL17681280M
Access and General Info:
- First Year Published: 1993
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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24Effects of wing leading-edge flap deflections on subsonic longitudinal aerodynamic characteristics of a wing-fuselage configuration with a 44ê swept wing
By William P Henderson
“Effects of wing leading-edge flap deflections on subsonic longitudinal aerodynamic characteristics of a wing-fuselage configuration with a 44ê swept wing” Metadata:
- Title: ➤ Effects of wing leading-edge flap deflections on subsonic longitudinal aerodynamic characteristics of a wing-fuselage configuration with a 44ê swept wing
- Author: William P Henderson
- Language: English
- Number of Pages: Median: 35
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Office - for sale by the National Technical Information Service
- Publish Date: 1978
- Publish Location: [Washington] - Springfield, Va
“Effects of wing leading-edge flap deflections on subsonic longitudinal aerodynamic characteristics of a wing-fuselage configuration with a 44ê swept wing” Subjects and Themes:
- Subjects: Leading edges (Aerodynamics) - Drag (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL17979145M - OL14932248M
Access and General Info:
- First Year Published: 1978
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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25Experimental trim drag values and flow-field measurements for a wide-body transport model with conventional and supercritical wings
By Peter F. Jacobs
“Experimental trim drag values and flow-field measurements for a wide-body transport model with conventional and supercritical wings” Metadata:
- Title: ➤ Experimental trim drag values and flow-field measurements for a wide-body transport model with conventional and supercritical wings
- Author: Peter F. Jacobs
- Language: English
- Publisher: ➤ National Aeronautics and Space Administation, Scientific and Technical Information Branch
- Publish Date: 1982
- Publish Location: [Washington, D.C.?]
“Experimental trim drag values and flow-field measurements for a wide-body transport model with conventional and supercritical wings” Subjects and Themes:
- Subjects: Transport planes - Drag (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL17832288M - OL17667067M
Access and General Info:
- First Year Published: 1982
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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26Experimental and computational ice shapes and resulting drag increase for a NACA 0012 airfoil
By Jaiwon Shin
“Experimental and computational ice shapes and resulting drag increase for a NACA 0012 airfoil” Metadata:
- Title: ➤ Experimental and computational ice shapes and resulting drag increase for a NACA 0012 airfoil
- Author: Jaiwon Shin
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - For sale by the National Technical Information Service
- Publish Date: 1992
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Experimental and computational ice shapes and resulting drag increase for a NACA 0012 airfoil” Subjects and Themes:
- Subjects: Icing (Meteorology) - Drag (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL16948964M - OL17676242M
Access and General Info:
- First Year Published: 1992
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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27Applications of a direct/iterative design method to complex transonic configurations
By Leigh Ann Smith
“Applications of a direct/iterative design method to complex transonic configurations” Metadata:
- Title: ➤ Applications of a direct/iterative design method to complex transonic configurations
- Author: Leigh Ann Smith
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1992
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Applications of a direct/iterative design method to complex transonic configurations” Subjects and Themes:
- Subjects: Transport planes - Drag (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL14686567M - OL17676903M
Access and General Info:
- First Year Published: 1992
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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28Full-scale wind-tunnel investigation of the advanced technology light twin-engine airplane (ATLIT)
By James L Hassell
“Full-scale wind-tunnel investigation of the advanced technology light twin-engine airplane (ATLIT)” Metadata:
- Title: ➤ Full-scale wind-tunnel investigation of the advanced technology light twin-engine airplane (ATLIT)
- Author: James L Hassell
- Language: English
- Number of Pages: Median: 209
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Office
- Publish Date: 1980
- Publish Location: ➤ Washington, D.C - [Springfield, Va
“Full-scale wind-tunnel investigation of the advanced technology light twin-engine airplane (ATLIT)” Subjects and Themes:
- Subjects: ➤ Airplanes - Handling characteristics - Control systems - Performance - Stability of airplanes - Drag (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL14932593M - OL17979305M
Access and General Info:
- First Year Published: 1980
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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29Drag of two-dimensional small-amplitude symmetric and asymmetric wavy walls in turbulent boundary layers
By John C Lin
“Drag of two-dimensional small-amplitude symmetric and asymmetric wavy walls in turbulent boundary layers” Metadata:
- Title: ➤ Drag of two-dimensional small-amplitude symmetric and asymmetric wavy walls in turbulent boundary layers
- Author: John C Lin
- Language: English
- Number of Pages: Median: 162
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
- Publish Date: 1984
- Publish Location: ➤ Washington, D.C - [Springfield, Va
“Drag of two-dimensional small-amplitude symmetric and asymmetric wavy walls in turbulent boundary layers” Subjects and Themes:
- Subjects: Aerodynamics - Turbulent boundary layer - Drag (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL17979799M - OL14933573M
Access and General Info:
- First Year Published: 1984
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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30Effect of afterbody geometry on aerodynamic characteristics of isolated nonaxisymmetric afterbodies at transonic Mach numbers
By Linda S. Bangert
“Effect of afterbody geometry on aerodynamic characteristics of isolated nonaxisymmetric afterbodies at transonic Mach numbers” Metadata:
- Title: ➤ Effect of afterbody geometry on aerodynamic characteristics of isolated nonaxisymmetric afterbodies at transonic Mach numbers
- Author: Linda S. Bangert
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1992
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Effect of afterbody geometry on aerodynamic characteristics of isolated nonaxisymmetric afterbodies at transonic Mach numbers” Subjects and Themes:
- Subjects: Fighter planes - Drag (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL17676904M - OL14686569M
Access and General Info:
- First Year Published: 1992
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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31Effects of tail span and empennage arrangement on drag of a typical single-engine fighter aft end
By James R. Burley
“Effects of tail span and empennage arrangement on drag of a typical single-engine fighter aft end” Metadata:
- Title: ➤ Effects of tail span and empennage arrangement on drag of a typical single-engine fighter aft end
- Author: James R. Burley
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
- Publish Date: 1986
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Effects of tail span and empennage arrangement on drag of a typical single-engine fighter aft end” Subjects and Themes:
- Subjects: Fighter planes - Drag (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL14664030M - OL17658849M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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32Flight-measured pressure characteristics of aft-facing steps in high Reyonlds number flow at Mach numbers of 2.20, 2.50, and 2.80 and comparison with other data
By Sheryll Goecke Powers
“Flight-measured pressure characteristics of aft-facing steps in high Reyonlds number flow at Mach numbers of 2.20, 2.50, and 2.80 and comparison with other data” Metadata:
- Title: ➤ Flight-measured pressure characteristics of aft-facing steps in high Reyonlds number flow at Mach numbers of 2.20, 2.50, and 2.80 and comparison with other data
- Author: Sheryll Goecke Powers
- Language: English
- Number of Pages: Median: 35
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Office - for sale by the National Technical Information Office
- Publish Date: 1978
- Publish Location: Springfield, Va - [Washington]
“Flight-measured pressure characteristics of aft-facing steps in high Reyonlds number flow at Mach numbers of 2.20, 2.50, and 2.80 and comparison with other data” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL17977016M - OL14925174M
Access and General Info:
- First Year Published: 1978
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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33Effect of several airframe/nozzle modifications on the drag of a variable-sweep bomber configuration
By Richard J. Re
“Effect of several airframe/nozzle modifications on the drag of a variable-sweep bomber configuration” Metadata:
- Title: ➤ Effect of several airframe/nozzle modifications on the drag of a variable-sweep bomber configuration
- Author: Richard J. Re
- Language: English
- Number of Pages: Median: 168
- Publisher: ➤ Fo r sale by the National Technical Information Service] - National Aeronautics and Space Administrat ion, Scientific and Technical Information Branch
- Publish Date: 1979
- Publish Location: ➤ Washington, D.C - [Springfield, Va
“Effect of several airframe/nozzle modifications on the drag of a variable-sweep bomber configuration” Subjects and Themes:
- Subjects: Testing - Drag (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL17798762M - OL17652571M
Access and General Info:
- First Year Published: 1979
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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34Modification in drag of turbulent boundary layers resulting from manipulation of large-scale structures
By T. C. Corke
“Modification in drag of turbulent boundary layers resulting from manipulation of large-scale structures” Metadata:
- Title: ➤ Modification in drag of turbulent boundary layers resulting from manipulation of large-scale structures
- Author: T. C. Corke
- Language: English
- Number of Pages: Median: 25
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1981
- Publish Location: ➤ Washington, D.C - [Springfield, Va
“Modification in drag of turbulent boundary layers resulting from manipulation of large-scale structures” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL17827911M - OL17654971M
Access and General Info:
- First Year Published: 1981
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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35Analytical and numerical investigation of structural response of compliant wall materials
By R. Balasubramanian
“Analytical and numerical investigation of structural response of compliant wall materials” Metadata:
- Title: ➤ Analytical and numerical investigation of structural response of compliant wall materials
- Author: R. Balasubramanian
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Office - for sale by the National Technical Information Service
- Publish Date: 1978
- Publish Location: Washington - Springfield, Va
“Analytical and numerical investigation of structural response of compliant wall materials” Subjects and Themes:
- Subjects: Skin friction (Aerodynamics) - Drag (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL17648019M - OL14930070M
Access and General Info:
- First Year Published: 1978
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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36Drag Reduction by Shock and Boundary Layer Control
By Egon Stanewsky, J. Delery, John Fulker and Paolo de Matteis

“Drag Reduction by Shock and Boundary Layer Control” Metadata:
- Title: ➤ Drag Reduction by Shock and Boundary Layer Control
- Authors: Egon StanewskyJ. DeleryJohn FulkerPaolo de Matteis
- Language: English
- Number of Pages: Median: 476
- Publisher: ➤ Springer London, Limited - Brand: Springer - Springer Berlin Heidelberg
- Publish Date: 2010 - 2013
“Drag Reduction by Shock and Boundary Layer Control” Subjects and Themes:
- Subjects: Drag (aerodynamics) - Shock waves
Edition Identifiers:
- The Open Library ID: OL28276803M - OL37102172M
- All ISBNs: 3642077625 - 9783540458562 - 3540458565 - 9783642077623
Access and General Info:
- First Year Published: 2010
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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37Aerodynamics of base combustion
By Workshop on Aerodynamics of Base Combustion Purdue University 1974.

“Aerodynamics of base combustion” Metadata:
- Title: ➤ Aerodynamics of base combustion
- Author: ➤ Workshop on Aerodynamics of Base Combustion Purdue University 1974.
- Language: English
- Number of Pages: Median: 522
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1976
- Publish Location: New York
“Aerodynamics of base combustion” Subjects and Themes:
- Subjects: Base flow (Aerodynamics) - Combustion - Congresses - Drag (Aerodynamics) - Wakes (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL8336222M - OL5207171M
- Online Computer Library Center (OCLC) ID: 1735520
- Library of Congress Control Number (LCCN): 75033380
- All ISBNs: 9780915928040 - 0915928043
Access and General Info:
- First Year Published: 1976
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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38Aerodynamic Drag Mechanisms of Bluff Bodies and Road Vehicles
By Gino Sovran

“Aerodynamic Drag Mechanisms of Bluff Bodies and Road Vehicles” Metadata:
- Title: ➤ Aerodynamic Drag Mechanisms of Bluff Bodies and Road Vehicles
- Author: Gino Sovran
- Language: English
- Publisher: Springer US - Island Press
- Publish Date: 1978
- Publish Location: Boston, MA
“Aerodynamic Drag Mechanisms of Bluff Bodies and Road Vehicles” Subjects and Themes:
- Subjects: Engineering - Mechanical engineering - Motor vehicles - Drag (aerodynamics)
Edition Identifiers:
- The Open Library ID: OL50675802M - OL27015426M
- Online Computer Library Center (OCLC) ID: 853259275
- All ISBNs: ➤ 9781468484366 - 1468484346 - 1468484354 - 9781468484359 - 9781468484342 - 1468484362
Access and General Info:
- First Year Published: 1978
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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39Kinetic theory of resistance in rarefied gases
By Marian Henrietta Heineman
“Kinetic theory of resistance in rarefied gases” Metadata:
- Title: ➤ Kinetic theory of resistance in rarefied gases
- Author: Marian Henrietta Heineman
- Language: English
- Publish Date: 1947
“Kinetic theory of resistance in rarefied gases” Subjects and Themes:
- Subjects: Rarefied gas dynamics - Drag (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL59170306M - OL59170303M
- Online Computer Library Center (OCLC) ID: 38471525
Access and General Info:
- First Year Published: 1947
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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40Some effects of base geometry on two dimensional base drag at subsonic and transonic speeds
By N. Pollock
“Some effects of base geometry on two dimensional base drag at subsonic and transonic speeds” Metadata:
- Title: ➤ Some effects of base geometry on two dimensional base drag at subsonic and transonic speeds
- Author: N. Pollock
- Language: English
- Number of Pages: Median: 19
- Publisher: ➤ Dept. of Supply, Australian Defence Scientific Service, Aeronautical Research Laboratories
- Publish Date: 1969
- Publish Location: Melbourne
“Some effects of base geometry on two dimensional base drag at subsonic and transonic speeds” Subjects and Themes:
- Subjects: Aerofoils - Drag (Aerodynamics) - Transonic Aerodynamics
Edition Identifiers:
- The Open Library ID: OL4370645M
- Library of Congress Control Number (LCCN): 78550585
Access and General Info:
- First Year Published: 1969
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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41A catalog of atmospheric densities from the drag on five artificial satellites
By Luigi G. Jacchia
“A catalog of atmospheric densities from the drag on five artificial satellites” Metadata:
- Title: ➤ A catalog of atmospheric densities from the drag on five artificial satellites
- Author: Luigi G. Jacchia
- Language: English
- Number of Pages: Median: 118
- Publisher: ➤ Smithsonian Institution, Astrophysical Observatory
- Publish Date: 1970
- Publish Location: Cambridge, Mass
“A catalog of atmospheric densities from the drag on five artificial satellites” Subjects and Themes:
- Subjects: Aerodynamics - Artificial satellites - Atmospheric density - Drag (Aerodynamics) - Tables
Edition Identifiers:
- The Open Library ID: OL4289402M
- Library of Congress Control Number (LCCN): 78316593
Access and General Info:
- First Year Published: 1970
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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42Viscous drag reduction
By Symposium on Viscous Drag Reduction Dallas 1968.
“Viscous drag reduction” Metadata:
- Title: Viscous drag reduction
- Author: ➤ Symposium on Viscous Drag Reduction Dallas 1968.
- Language: English
- Number of Pages: Median: 500
- Publisher: Plenum Press
- Publish Date: 1969
- Publish Location: New York
“Viscous drag reduction” Subjects and Themes:
- Subjects: Congresses - Drag (Aerodynamics) - Fluid mechanics
Edition Identifiers:
- The Open Library ID: OL4563161M
- Online Computer Library Center (OCLC) ID: 18635
- Library of Congress Control Number (LCCN): 77076496
Access and General Info:
- First Year Published: 1969
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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43Rotorcraft parasite drag
By American Helicopter Society. Ad Hoc Committee on Rotorcraft Parasite Drag.
“Rotorcraft parasite drag” Metadata:
- Title: Rotorcraft parasite drag
- Author: ➤ American Helicopter Society. Ad Hoc Committee on Rotorcraft Parasite Drag.
- Language: English
- Number of Pages: Median: 108
- Publisher: The Committee
- Publish Date: 1975
- Publish Location: Washington
“Rotorcraft parasite drag” Subjects and Themes:
- Subjects: Aerodynamics - Drag (Aerodynamics) - Helicopters
Edition Identifiers:
- The Open Library ID: OL4475657M
- Library of Congress Control Number (LCCN): 79303196
Access and General Info:
- First Year Published: 1975
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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44The upper atmosphere and satellite drag
By R. J. Stirton
“The upper atmosphere and satellite drag” Metadata:
- Title: ➤ The upper atmosphere and satellite drag
- Author: R. J. Stirton
- Language: English
- Number of Pages: Median: 15
- Publisher: Smithsonian Institution
- Publish Date: 1960
- Publish Location: Washington
“The upper atmosphere and satellite drag” Subjects and Themes:
- Subjects: Artificial satellites - Drag (Aerodynamics) - Upper Atmosphere
Edition Identifiers:
- The Open Library ID: OL5814931M
- Online Computer Library Center (OCLC) ID: 613259
- Library of Congress Control Number (LCCN): 60062069
Access and General Info:
- First Year Published: 1960
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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45An experimental investigation of the influence of base bleed on the base drag of various propelling nozzle configurations
By Roberts, J. B. writer on aerodynamics.
“An experimental investigation of the influence of base bleed on the base drag of various propelling nozzle configurations” Metadata:
- Title: ➤ An experimental investigation of the influence of base bleed on the base drag of various propelling nozzle configurations
- Author: ➤ Roberts, J. B. writer on aerodynamics.
- Language: English
- Number of Pages: Median: 25
- Publisher: H.M.S.O.
- Publish Date: 1967
- Publish Location: London
“An experimental investigation of the influence of base bleed on the base drag of various propelling nozzle configurations” Subjects and Themes:
- Subjects: Drag (Aerodynamics) - Supersonic nozzles
Edition Identifiers:
- The Open Library ID: OL5579907M
- Library of Congress Control Number (LCCN): 67093871
Access and General Info:
- First Year Published: 1967
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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46Flight measurements of the lift, longitudinal trim and drag of the Fairey Delta 2 at mach numbers up to 1.65 and comparisons with wind-tunnel results
By R. Rose
“Flight measurements of the lift, longitudinal trim and drag of the Fairey Delta 2 at mach numbers up to 1.65 and comparisons with wind-tunnel results” Metadata:
- Title: ➤ Flight measurements of the lift, longitudinal trim and drag of the Fairey Delta 2 at mach numbers up to 1.65 and comparisons with wind-tunnel results
- Author: R. Rose
- Language: English
- Number of Pages: Median: 57
- Publisher: H.M.S.O.
- Publish Date: 1969
- Publish Location: London
“Flight measurements of the lift, longitudinal trim and drag of the Fairey Delta 2 at mach numbers up to 1.65 and comparisons with wind-tunnel results” Subjects and Themes:
- Subjects: ➤ Airplanes - Drag (Aerodynamics) - Flight testing - Lift (Aerodynamics) - Triangular Wings - Fairey Delta (Supersonic plane) - Airplanes, wings - Drag (aerodynamics) - Lift (aerodynamics) - Airplanes, flight testing
Edition Identifiers:
- The Open Library ID: OL4366710M
- Online Computer Library Center (OCLC) ID: 73239
- Library of Congress Control Number (LCCN): 78463325
- All ISBNs: 0114701962 - 9780114701963
Access and General Info:
- First Year Published: 1969
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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47Theoretical/numerical study of feasibility of use of winglets on low aspect ratio wings at subsonic and transonic Mach numbers to reduce drag
By John M. Kuhlman
“Theoretical/numerical study of feasibility of use of winglets on low aspect ratio wings at subsonic and transonic Mach numbers to reduce drag” Metadata:
- Title: ➤ Theoretical/numerical study of feasibility of use of winglets on low aspect ratio wings at subsonic and transonic Mach numbers to reduce drag
- Author: John M. Kuhlman
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Division - For sale by the National Technical Information Service]
- Publish Date: 1988
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Theoretical/numerical study of feasibility of use of winglets on low aspect ratio wings at subsonic and transonic Mach numbers to reduce drag” Subjects and Themes:
- Subjects: Drag (Aerodynamics) - Transonic Aerodynamics
Edition Identifiers:
- The Open Library ID: OL15284519M
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
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48Short-cowl front-fan turbojets; friction drag and wall-jet effects on cylindrical afterbodies
By John Edward Green
“Short-cowl front-fan turbojets; friction drag and wall-jet effects on cylindrical afterbodies” Metadata:
- Title: ➤ Short-cowl front-fan turbojets; friction drag and wall-jet effects on cylindrical afterbodies
- Author: John Edward Green
- Language: English
- Number of Pages: Median: 23
- Publisher: H.M.S.O.
- Publish Date: 1969
- Publish Location: London
“Short-cowl front-fan turbojets; friction drag and wall-jet effects on cylindrical afterbodies” Subjects and Themes:
- Subjects: ➤ Air jets - Airplanes - Drag (Aerodynamics) - Turbojet engines - Drag (aerodynamics) - Airplanes, turbojet engines - Jet planes
Edition Identifiers:
- The Open Library ID: OL5324809M
- Online Computer Library Center (OCLC) ID: 379644
- Library of Congress Control Number (LCCN): 72177580
- All ISBNs: 9780114701765 - 0114701768
Access and General Info:
- First Year Published: 1969
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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49The pressure drag of an aerofoil with six different round leading edges, at transonic and low supersonic speeds
By P. G. Wilby
“The pressure drag of an aerofoil with six different round leading edges, at transonic and low supersonic speeds” Metadata:
- Title: ➤ The pressure drag of an aerofoil with six different round leading edges, at transonic and low supersonic speeds
- Author: P. G. Wilby
- Language: English
- Publisher: H.M.S.O.
- Publish Date: 1967
- Publish Location: London
“The pressure drag of an aerofoil with six different round leading edges, at transonic and low supersonic speeds” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL5578690M
- Library of Congress Control Number (LCCN): 67091817
Access and General Info:
- First Year Published: 1967
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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50Drag on a body in nearly-free molecular flow
By Marian H. Rose

“Drag on a body in nearly-free molecular flow” Metadata:
- Title: ➤ Drag on a body in nearly-free molecular flow
- Author: Marian H. Rose
- Language: English
- Number of Pages: Median: 61
- Publisher: ➤ Creative Media Partners, LLC - Courant Institute of Mathematical Sciences, New York University
- Publish Date: 1963 - 2015
- Publish Location: New York
“Drag on a body in nearly-free molecular flow” Subjects and Themes:
- Subjects: Gas flow - Drag (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL39064498M - OL17866843M
- Online Computer Library Center (OCLC) ID: 62529705
- All ISBNs: 1340290146 - 9781340290146
Access and General Info:
- First Year Published: 1963
- 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
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Wiki
Source: Wikipedia
Wikipedia Results
Search Results from Wikipedia
Drag (physics)
waves. Last, in aerodynamics the term "parasitic drag" is often used. Parasitic drag is the sum of form drag and skin friction drag and is entirely negative
Automotive aerodynamics
Automotive aerodynamics is the study of the aerodynamics of road vehicles. Its main goals are reducing drag and wind noise, minimizing noise emission,
Lift-to-drag ratio
In aerodynamics, the lift-to-drag ratio (or L/D ratio) is the lift generated by an aerodynamic body such as an aerofoil or aircraft, divided by the aerodynamic
Aerodynamics
study of aerodynamics began in the modern sense in the eighteenth century, although observations of fundamental concepts such as aerodynamic drag were recorded
Automobile drag coefficient
The drag coefficient is a common measure in automotive design as it pertains to aerodynamics. Drag is a force that acts parallel to and in the same direction
Lift-induced drag
Lift-induced drag, induced drag, vortex drag, or sometimes drag due to lift, in aerodynamics, is an aerodynamic drag force that occurs whenever a moving
Drag coefficient
Clancy, L. J.: Aerodynamics. Section 11.17 Hoerner, Sighard F. (1965). Fluid-Dynamic Drag : Practical Information on Aerodynamic Drag and Hydrodynamic
Drag curve
The drag curve or drag polar is the relationship between the drag on an aircraft and other variables, such as lift, the coefficient of lift, angle-of-attack
Parasitic drag
{Re}}}} NACA duct Jet engine ram drag Skin friction line Anderson, John D. Jr. (1991). Fundamentals of aerodynamics (2nd ed.). New York: McGraw-Hill.
Ground effect (aerodynamics)
In aircraft, the ground effect is the reduced aerodynamic drag that an aircraft's wings generate when they are close to a surface (land or water). Ground