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Tables
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Aerodynamics Supersonic
Subject: Is
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Drag (Aerodynamics)

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Online Results (34)
1.
The natural flow wing-design concept
Author
Wood, Richard M.
Published
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
2.
The natural flow wing-design concept
Author
Wood, Richard M.
Published
[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : For sale by the National Technical Information Service], 1992.
Location
SML, Microform (Non-Circulating) >> NAS 1.60:3193
Format
Books / Microforms
3.
The effects of winglets on low aspect ratio wings at supersonic Mach numbers
Author
Keenan, James A. (James Anthony), 1966-
Published
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; Springfield, Va. : For sale by the National Technical Information Service, 1991.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
4.
Experimental investigation of porous-floor effects on cavity flow fields at supersonic speeds
Author
Wilcox, Floyd J. (Floyd Jay)
Published
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
5.
Planform effects on the supersonic aerodynamics of multibody configurations
Author
McMillin, S. Naomi (Susan Naomi)
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1987.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
6.
An experimental and analytical study of the aerodynamic interference effects between two Sears-Haack bodies at Mach 2.7
Author
Bantle, Jeffrey W.
Published
Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1985.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
7.
Effect of nonlifting empennage surfaces on single-engine afterbody/nozzle drag at Mach numbers from 0.5 to 2.2
Author
Berrier, Bobby L.
Published
Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
8.
Effect of nonlifting empennage surfaces on single-engine afterbody/nozzle drag at Mach numbers from 0.5 to 2.2
Author
Berrier, Bobby L.
Published
Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977.
Location
Library Shelving Facility (LSF) >> NASA TN D-8326
Format
Books
9.
Effects of roughness size on the position of boundary-layer transition and on the aerodynamic characteristics of a 55 ̊swept delta wing at supersonic speeds
Author
Stallings, Robert L.
Published
[Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : for sale by the National Technical Information Service, 1977.
Location
SML, Microform (Non-Circulating) >> NAS 1.60:1027
Format
Books / Microforms
10.
Effects of roughness size on the position of boundary-layer transition and on the aerodynamics characteristics of a 55 ̊swept delta wing at supersonic speeds
Author
Stallings, Robert L.
Published
[Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1977.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
11.
Drag and stability characteristics of a variety of reefed and unreefed parachute configurations at Mach 1.80 with an empirical correlation for supersonic Mach numbers
Author
Couch, Lana M.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
12.
Drag and stability characteristics of a variety of reefed and unreefed parachute configurations at Mach 1.80 with an empirical correlation for supersonic Mach numbers
Author
Couch, Lana M.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975.
Location
Library Shelving Facility (LSF) >> NASA TR-R 429
Format
Books
13.
Deployment and performance characteristics of 1.5-meter supersonic attached inflatable decelerators
Author
Bohon, Herman L.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
14.
Deployment and performance characteristics of 1.5-meter supersonic attached inflatable decelerators
Author
Bohon, Herman L.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974.
Location
Library Shelving Facility (LSF) >> NASA TN D-7550
Format
Books
15.
Numerical methods for the design and analysis of wings at supersonic speeds
Author
Carlson, Harry W.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
16.
Numerical methods for the design and analysis of wings at supersonic speeds
Author
Carlson, Harry W.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974.
Location
Library Shelving Facility (LSF) >> NASA TN D-7713
Format
Books
17.
Sweep effect on the drag of rows of perpendicular circular cylinders in a laminar boundary layer at supersonic free-stream velocities
Author
Lamb, Milton
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
18.
Sweep effect on the drag of rows of perpendicular circular cylinders in a laminar boundary layer at supersonic free-stream velocities
Author
Lamb, Milton
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974.
Location
Library Shelving Facility (LSF) >> NASA TN D-7812
Format
Books
19.
Drag characteristics of circular cylinders in a laminar boundary layer at supersonic free-stream velocities
Author
Stallings, Robert L.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973.
Location
Library Shelving Facility (LSF) >> NASA TN D-7369
Format
Books
20.
Numerical method for design of minimum-drag supersonic wing camber with constraints on pitching moment and surface deformation
Author
Sorrells, Russell B.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972.
Location
Library Shelving Facility (LSF) >> NASA TN D-7097
Format
Books
21.
Calculated pressure distributions and components of total-drag coefficients for 18 constant-volume slender bodies of revolution at zero incidence for Mach numbers from 2.0 to 12.0, with experimental aerodynamic characteristics for three of the bodies
Author
Stiver, Louis S.
Published
Washington, D.C. : National Aeronautics and Space Administration, 1971.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
22.
Calculated pressure distributions and components of total-drag coefficients for 18 constant-volume slender bodies of revolution at zero incidence for Mach numbers from 2.0 to 12.0, with experimental aerodynamic characteristics for three of the bodies
Author
Stiver, Louis S.
Published
Washington, D.C. : National Aeronautics and Space Administration, 1971.
Location
Library Shelving Facility (LSF) >> NASA TN D-6536
Format
Books
23.
An approximate solution of additive-drag coefficient and mass-flow ratio for inlets utilizing right circular cones at zero angle of attack
Author
Mascitti, Vincent R.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
24.
An approximate solution of additive-drag coefficient and mass-flow ratio for inlets utilizing right circular cones at zero angle of attack
Author
Mascitti, Vincent R. (Vincent Robert), 1941-
Published
Washington, D.C. : National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969.
Location
Library Shelving Facility (LSF) >> NASA TN D-5537
Format
Books
25.
Charts of additive drag coefficient and mass-flow ratio for inlets utilizing right circular cones at zero angle of attack
Author
Mascitti, Vincent R. (Vincent Robert), 1941-
Published
Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 20230], 1966.
Location
Library Shelving Facility (LSF) >> NASA TN D-3434
Format
Books