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Hugh L. Dryden Flight Research Center,
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1
Extension of Ko straight-beam displacement theory to deformed shape predictions of slender curved structures
by
William L. Ko.
Published: National Aeronautics and Space Administration, Dryden Flight Research Center, 2011
Description: 1 online resource (vii, 76 pages) : illustrations.
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2
Applications of Ko displacement theory to the deformed shape predictions of the doubly-tapered Ikhana wing
by
Ko, William L.
Published: National Aeronautics and Space Administration, Dryden Flight Research Center, 2009
Description: 1 online resource (v, 23 pages) : illustrations.
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3
Further development of Ko displacement theory for deformed shape predictions of nonuniform aerospace structures
by
Ko, William L.
Published: National Aeronautics and Space Administration, Dryden Flight Research Center, 2009
Description: 1 online resource (iv, 79 pages) : illustrations.
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4
X-1 paper glider kit investigating the basics of flight with a model of the first supersonic aircraft
Published: National Aeronautics and Space Administration, [Dryden Flight Research Center], 2000
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5
X-Gliders exploring flight research with experimental gliders
Published: National Aeronautics and Space Administration, [Dryden Flight Research Center], 1999
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6
Centennial of flight, 1903-2003
Published: National Aeronautics and Space Administration, Dryden Flight Research Center, 2002
Description: 9 photographs : color ; 22 x 28 cm.
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7
Methods for in-flight wing shape predictions of highly flexible unmanned aerial vehicles formulation of Ko displacement theory
by
Ko, William L.
Published: National Aeronautics and Space Administration, Dryden Flight Research Center, 2010
Description: 1 online resource (20 pages) : illustrations.
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8
Improved displacement transfer functions for structure deformed shape predictions using discretely distributed surface strains
by
Ko, William L.,
Published: National Aeronautics and Space Administration, Dryden Flight Research Center, 2012
Description: 1 online resource (vi, 79 pages) : illustrations (some color).
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9
First- and second-order displacement transfer functions for structural shape calculations using analytically predicted surface strains
by
Ko, William L.,
Published: National Aeronautics and Space Administration, Dryden Flight Research Center, 2012
Description: 1 online resource (vi, 51 pages) : illustrations.
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10
A modified T-value method for selection of strain gages for measuring loads on a low aspect ratio wing
by
Tang, Ming Han, 1939-
Published: NASA Dryden Flight Research Center, 1980
Description: 1 online resource (51 pages) : illustrations.
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11
Development and flight test of an emergency flight control system using only engine thrust on an MD-11 transport airplane
by
Burcham, Frank W.,
Published: National Aeronautics and Space Administration, Dryden Flight Research Center, 1997
Description: 1 online resource (xiii, 133 pages) : color illustrations.
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12
Deformed shape calculation of a full-scale wing using fiber optic strain data from a ground loads test
by
Jutte, Christine V.,
Published: National Aeronautics and Space Administration, Dryden Flight Research Center, 2011
Description: 1 online resource (vi, 50 pages) : color illustrations.
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13
User's manual for MMLE3, a general FORTRAN program for maximum likelihood parameter estimation
by
Maine, Richard E.,
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980
Description: 1 online resource (iv, 85 pages) : illustrations.
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14
In-flight boundary-layer measurements on a hollow cylinder at a Mach number of 3.0
by
Quinn, Robert D.,
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980
Description: 1 online resource (49 pages) : illustrations.
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15
Flight evaluation of a simplified gross thrust calculation technique using an F100 turbofan engine in an F-15 airplane
by
Kurtenbach, Frank J.,
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1981
Description: 1 online resource (18 pages) : illustrations.
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16
Important factors in the maximum likelihood analysis of flight test maneuvers
by
Iliff, Kenneth W.,
Published: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1979
Description: 1 online resource (iii, 40 pages) : illustrations.
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17
Effects of inlet distortion on a static pressure probe mounted on the engine hub in an F-15 airplane
by
Hughes, Donald L. 1926-
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985
Description: 1 online resource (20 pages) : illustrations.
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