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Aerodynamics, Hypersonic

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1.
X-15 : extending the frontiers of flight
Author
Jenkins, Dennis R
Published
Washington DC : NASA, [2007]
Online
Online book
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2.
Facing the heat barrier : a history of hypersonics
Author
Heppenheimer, T. A., 1947-
Published
Washington, DC : NASA, [2006]
Online
Online book
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3.
Enhancing U.S. competitiveness : NASA hypersonics research and wind tunnel programs : hearing before the Subcommittee on Technology, Environment, and Aviation of the Committee on Science, Space, and Technology, U.S. House of Representatives, One Hundred Third Congress, second session, March 15, 1994
Author
United States. Congress. House. Committee on Science, Space, and Technology. Subcommittee on Technology, Environment, and Aviation
Published
Washington : U.S. G.P.O. : For sale by the U.S. G.P.O., Supt. of Docs., Congressional Sales Office, 1994.
Online
4.SCI 2:103/98
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4.
An analysis of combustion studies in shock expansion tunnels and reflected shock tunnels
Author
Jachimowski, Casimir J.
Published
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.
Online
Online book
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5.
Flow analysis and design optimization methods for nozzle afterbody of a hypersonic vehicle
Author
Baysal, Oktay
Published
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.
Online
Online book
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6.
A simplified method for thermal analysis of a cowl leading edge subject to intense local shock-wave-interference heating
Author
McGowan, David M.
Published
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.
Online
Online book
Location
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7.
Simulation of real-gas effects on pressure distributions for aeroassist flight experiment vehicle and comparison with prediction
Author
Micol, John R.
Published
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.
Online
Online book
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8.
Aerothermal test results from the first flight of the Pegasus air-launched space booster
Published
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.
Online
Online book
Location
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9.
Evaluation of a technique to generate artificially thickened boundary layers in supersonic and hypersonic flows
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
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10.
An explicit upwind algorithm for solving the parabolized Navier-Stokes equations
Author
Korte, John J.
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, 1991.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
11.
NASA Aerodynamics Program : annual report 1990
Published
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.
Online
Online book
Location
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12.
Nonparallel instability of supersonic and hypersonic boundary layers
Author
El-Hady, Nabil M.
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, 1991.
Online
Online book
Location
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13.
Parametric experimental investigation of a scramjet nozzle at Mach 6 with freon and argon or air used for exhaust simulation
Author
Cubbage, James M.
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, 1991.
Online
Online book
Location
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Books / Online
14.
An upwind-biased space marching algorithm for supersonic viscous flow
Author
Greene, Francis A.
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, 1991.
Online
Online book
Location
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Books / Online
15.
Viscous computations of cold air/air flow around scramjet nozzle afterbody
Author
Baysal, Oktay
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
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16.
Aerodynamic pressure and heating-rate distributions in tile gaps around chine regions with pressure at a Mach number of 6.6
Author
Hunt, L. Roane (Lewis Roane)
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
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Books / Online
17.
An approximate method for calculating three-dimensional inviscid hypersonic flow fields
Author
Riley, Christopher J. (Christopher Joseph), 1964-
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
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Books / Online
18.
Flow separation in shock wave boundary layer interactions at hypersonic speeds
Author
Hamed, A. (Awatef)
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
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Books / Online
19.
Improved tangent-cone method for the Aerodynamic Preliminary Analysis System (APAS) version of the Hypersonic Arbitrary-Body Program
Author
Cruz, Christopher I.
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
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Books / Online
20.
Measured and predicted aerodynamic coefficients and shock shapes for Aeroassist Flight Experiment (AFE) configuration
Author
Wells, William L.
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
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Books / Online
21.
Real-time aerodynamic heating and surface temperature calculations for hypersonic flight simulation
Author
Quinn, Robert D.
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
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Books / Online
22.
An upwind-biased, point-implicit relaxation algorithm for viscous, compressible perfect-gas flows
Author
Gnoffo, Peter A.
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
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23.
Conservation equations and physical models for hypersonic air flows in thermal and chemical nonequilibrium
Author
Gnoffo, Peter A.
Published
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
Online
Online book
Location
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Books / Online
24.
Fluctuating pressures measured beneath a high-temperature, turbulent boundary layer on a flat plate at a Mach number of 5
Author
Parrott, Tony L.
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, 1989.
Online
Online book
Location
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Format
Books / Online
25.
Aerodynamic characteristics of wings designed with a combined-theory method to cruise at a Mach number of 4.5
Author
Mack, Robert J.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1988.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online