Langley Research Center
The Langley Research Center (LaRC or NASA Langley), located in Hampton, Virginia, near the Chesapeake Bay front of Langley Air Force Base, is the oldest of NASA's field centers. LaRC has focused primarily on aeronautical research but has also tested space hardware such as the Apollo Lunar Module. In addition, many of the earliest high-profile space missions were planned and designed on-site. Langley was also considered a potential site for NASA's Manned Spacecraft Center prior to the eventual selection of Houston, Texas.Established in 1917 by the National Advisory Committee for Aeronautics (NACA), the research center devotes two-thirds of its programs to aeronautics and the rest to space. LaRC researchers use more than 40 wind tunnels to study and improve aircraft and spacecraft safety, performance, and efficiency. Between 1958 and 1963, when NASA (the successor agency to NACA) started Project Mercury, LaRC served as the main office of the Space Task Group.
In September 2019, after previously serving as associate director and deputy director, Clayton P. Turner was appointed director of NASA Langley. Provided by Wikipedia
Showing 1 - 20 results of 8,344 for search 'Langley Research Center', query time: 0.10s
Refine Results
-
1
A study of the application of heat or force fields to the sonic-boom-minimization problem / by Miller, David S. (Of Langley Research Center)
Published 1969Call Number: Loading…
Located: Loading…Government Document Book Loading… -
2
Numerical method for design of minimum-drag supersonic wing camber with constraints on pitching moment and surface deformation / by Sorrells, Russell B., Miller, David S. (Of Langley Research Center)
Published 1972“…Langley Research Center…”
Call Number: Loading…Online Access
Located: Loading…
Government Document eBook -
3
Lee-side flow over delta wings at supersonic speeds / by Miller, David S. (Of Langley Research Center), Wood, Richard M.
Published 1985“…Langley Research Center…”
Call Number: Loading…Online Access
Located: Loading…
Government Document eBook -
4
Theoretical and experimental investigation of supersonic aerodynamic characteristics of a twin-fuselage concept by Wood, Richard M., Miller, David S. (Of Langley Research Center), Brentner, Kenneth S.
Published 1983Call Number: Loading…
Located: Loading…Government Document Microfilm Book Loading… -
5
Theoretical and experimental investigation of supersonic aerodynamic characteristics of a twin-fuselage concept / by Wood, Richard M., Miller, David S. (Of Langley Research Center), Brentner, Kenneth S.
Published 1983Call Number: Loading…Online Access
Located: Loading…
Government Document eBook -
6
Theoretical and experimental investigation of supersonic aerodynamic characteristics of a twin-fuselage concept / by Wood, Richard M., Miller, David S. (Of Langley Research Center), Brentner, Kenneth S.
Published 1983Call Number: Loading…Search for the full-text version of this title in HathiTrust
Located: Loading…
Government Document Book -
7
Numerical methods for the design and analysis of wings at supersonic speeds by Carlson, Harry W.
Published 1974Other Authors: “…David S. (Of Langley Research Center)…”
Call Number: Loading…
Located: Loading…Government Document Book Loading… -
8
Wing planform effects at supersonic speeds for an advanced fighter configuration / by Wood, Richard M.
Published 1984Other Authors: “…David S. (Of Langley Research Center)…”
Call Number: Loading…Search for the full-text version of this title in HathiTrust
Located: Loading…
Government Document Book -
9
Experimental investigation of leading-edge thrust at supersonic speeds / by Wood, Richard M.
Published 1983Other Authors: “…David S. (Of Langley Research Center)…”
Call Number: Loading…Search for the full-text version of this title in HathiTrust
Located: Loading…
Government Document Book -
10
Pressure and force data for a flat wing and a warped conical wing having a shockless recompression at Mach 1.62 /
Published 1981Other Authors: “…David S. (Of Langley Research Center)…”
Call Number: Loading…Search for the full-text version of this title in HathiTrust
Located: Loading…
Government Document Book -
11
Effect of fuselage upwash on the supersonic longitudinal aerodynamic characteristics of two fighter configurations / by Wood, Richard M.
Published 1984Other Authors: “…David S. (Of Langley Research Center)…”
Call Number: Loading…Search for the full-text version of this title in HathiTrust
Located: Loading…
Government Document Book -
12
Numerical method for design of minimum-drag supersonic wing camber with constraints on pitching moment and surface deformation / by Sorrells, Russell B.
Published 1972Other Authors: “…David S. (Of Langley Research Center)…”
Call Number: Loading…
Located: Loading…Government Document Book Loading… -
13
Aerodynamic characteristics at Mach numbers of 1.5, 1.8, and 2.0 of a blended wing-body configuration with and without integral canards / by Robins, A. Warner
Published 1979Other Authors: “…David S. (Of Langley Research Center)…”
Call Number: Loading…Search for the full-text version of this title in HathiTrust
Located: Loading…
Government Document Book -
14
Body and canard effects on an attached-flow maneuver wing at Mach 1.62 / by Pittman, Jimmy L.
Published 1984Other Authors: “…David S. (Of Langley Research Center)…”
Call Number: Loading…Search for the full-text version of this title in HathiTrust
Located: Loading…
Government Document Book -
15
A non-dissipative staggered fourth-order accurate explicit finite difference scheme for the time-domain Maxwell's equations by Yeffet, Amir
Published 1999“…Langley Research Center…”
Call Number: Loading…
Located: Loading…Government Document Microfilm Book Loading… -
16
Investigation of a technique for measuring dynamic ground effect in a subsonic wind tunnel by Graves, Sharon S.
Published 1999“…Langley Research Center…”
Call Number: Loading…view full text online
Located: Loading…
Government Document Microfilm Book -
17
Parallel implementation of the discontinuous Galerkin method by Baggag, Abdelkader
Published 1999“…Langley Research Center…”
Call Number: Loading…view full text online
Located: Loading…
Government Document Microfilm Book -
18
Parallelization of a multigrid incompressible viscous cavity flow solver using openMP by Roe, Kevin
Published 1999“…Langley Research Center…”
Call Number: Loading…Click here to view full text online
Located: Loading…
Government Document Microfilm Book -
19
Advances in composites technology by Tenney, Darrel R.
Published 1985“…Langley Research Center…”
Call Number: Loading…
Located: Loading…Government Document Book Loading… -
20
Cyclic cryogenic thermal-mechanical testing of an X-33/RLV liquid oxygen tank concept by Rivers, H. Kevin
Published 1999“…Langley Research Center…”
Call Number: Loading…
Located: Loading…Government Document Microfilm Book Loading…
Search Tools:
RSS Feed
–
Save Search
Related Subjects
Airplanes
Mathematical models
Aerodynamics
Testing
Computer programs
Space vehicles
Composite materials
Design and construction
Noise
Measurement
Wings
Finite element method
Wind tunnel tests
Computational fluid dynamics
Aerodynamics, Supersonic
Computer simulation
Algorithms
Wind tunnels
Materials
Control systems
Boundary layer
Turbulence
Fluid dynamics
Aerodynamics, Hypersonic
Aeroelasticity
Helicopters
Aerodynamics, Transonic
Heat
Space shuttles
Numerical analysis