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Author/Creator: Is
Is Is Not
Langley Research Center
Subject: Is
Is Is Not
Aerodynamics, Hypersonic

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Online Results (2)
1.
H-P adaptive methods for finite element analysis of aerothermal loads in high-speed flows
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
Location
SML, Microform (Non-Circulating) >> NAS 1.26:189739
Format
Books / Microforms
2.
Reynolds number influences in aeronautics
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1993]
Location
SML, Microform (Non-Circulating) >> NAS 1.15:107730
Format
Books / Microforms
3.
Shock tunnel studies for scramjet phenomena, supplement 6
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
Location
SML, Microform (Non-Circulating) >> NAS 1.26:191428
Format
Books / Microforms
4.
Heat transfer characteristics of hypersonic waveriders with an emphasis on the leading edge effects
Author
Vanmol, Denis O.
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Center, distributor, 1992]
Location
SML, Microform (Non-Circulating) >> NAS 1.26:189586
Format
Books / Microforms
5.
A High angle of attack inviscid shuttle orbiter computation
Author
Kleb, William L.
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1992]
Location
SML, Microform (Non-Circulating) >> NAS 1.15:107606
Format
Books / Microforms
6.
Hypersonic vehicle control law development using H[infinity symbol] and [mu]-synthesis
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1992]
Location
SML, Microform (Non-Circulating) >> NAS 1.15:107689
Format
Books / Microforms
7.
Studies of shock/shock interaction on smooth and transpiration-cooled hemispherical nosetips in hypersonic flow
Author
Holden, Michael S.
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1992]
Location
SML, Microform (Non-Circulating) >> NAS 1.26:189585
Format
Books / Microforms
8.
A study of viscous interaction effects on hypersonic waveriders
Author
Chang, Jinhwa
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va.? : National Technical Information Service, distributor, 1992]
Location
SML, Microform (Non-Circulating) >> NAS 1.26:189587
Format
Books / Microforms
9.
Addition of equilibrium air to an upwind Navier-Stokes code and other first steps toward a more generalized flow solver
Author
Rosen, Bruce S.
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1991]
Location
SML, Microform (Non-Circulating) >> NAS 1.15:102616
Format
Books / Microforms
10.
An approximate viscous shock layer technique for calculating chemically reacting hypersonic flows about blunt-nosed bodies
Author
Cheatwood, F. McNeil
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
Location
SML, Microform (Non-Circulating) >> NAS 1.26:187617
Format
Books / Microforms
11.
Effects of Görtler vortices, wall cooling and gas dissociation on the Rayleigh instability in a hypersonic boundary layer
Author
Fu, Yibin
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
Location
SML, Microform (Non-Circulating) >> NAS 1.26:189577
Format
Books / Microforms
12.
Investigation of nose bluntness and angle of attack effects on slender bodies in viscous hypertension flows
Author
Sehgal, A. K.
Published
Norfolk, Va. : Dept. of Mechanical Engineering & Mechanics, College of Engineering & Technology, Old Dominion University ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
Location
SML, Microform (Non-Circulating) >> NAS 1.26:188153
Format
Books / Microforms
13.
Multigrid for hypersonic viscous two-and three-dimensional flows
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
Location
SML, Microform (Non-Circulating) >> NAS 1.26:187603
Format
Books / Microforms
14.
Nonlinear development and secondary instability of Görtler vortices in hypersonic flows
Author
Fu, Yibin B.
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1991]
Location
SML, Microform (Non-Circulating) >> NAS 1.26:187563
Format
Books / Microforms
15.
Nonlinear instability of hypersonic flow past a wedge
Author
Seddougui, Sharon O.
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
Location
SML, Microform (Non-Circulating) >> NAS 1.26:187609
Format
Books / Microforms
16.
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]
Location
SML, Microform (Non-Circulating) >> NAS 1.26:4373
Format
Books / Microforms
17.
Progress with multigrid schemes for hypersonic flow problems
Author
Radespiel, R.
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
Location
SML, Microform (Non-Circulating) >> NAS 1.26:189579
Format
Books / Microforms
18.
Studies of aerothermal loads generated in regions of shock/shock interaction in hypersonic flow
Author
Holden, Michael S.
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributors, 1991]
Location
SML, Microform (Non-Circulating) >> NAS 1.26:181893
Format
Books / Microforms
19.
Effects of nose bluntness and shock-shock interactions on blunt bodies in viscous hypersonic flows progress report for the period ended December 31, 1989
Author
Singh, D. J.
Published
Norfolk, Va. : Old Dominion University Research Foundation ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
Online
http://purl.access.gpo.gov/GPO/LPS63194
Location
Yale Internet Resource
Format
Books / Online / Microforms
20.
Multigrid for hypersonic inviscid flows
Author
Decker, Naomi H.
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990]
Location
SML, Microform (Non-Circulating) >> NAS 1.26:182082
Format
Books / Microforms
21.
Hypersonic nozzle design final report
Author
Griffith, Wayland C.
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1989]
Location
SML, Microform (Non-Circulating) >> NAS 1.26:186261
Format
Books / Microforms
22.
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.
Location
Library Shelving Facility (LSF) >> NAS 1.60:2799
Format
Books
23.
Compendium of NASA Langley reports on hypersonic aerodynamics
Author
Sabo, Frances E.
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1987]
Location
SML, Microform (Non-Circulating) >> NAS 1.15:87760
Format
Books / Microforms
24.
Mach 6 experimental and theoretical stability and performance of a cruciform missile at angles of attack up to 65⁰
Author
Hartman, Edward R.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1987.
Location
Library Shelving Facility (LSF) >> NAS 1.60:2733
Format
Books
25.
Modification to the Langley 8-foot high temperature tunnel for hypersonic propulsion testing
Author
Reubush, David E.
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1987]
Location
SML, Microform (Non-Circulating) >> NAS 1.15:100486
Format
Books / Microforms