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Investigation of a technique for measuring dynamic ground effect in a subsonic wind tunnel [microform] / Sharon S. Graves.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
1999
0 resources
Numerical analysis of tangential slot blowing on a generic chined forebody [microform] / Roxana M. Agosta.
Text
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
Flutter analysis of supersonic axial flow cascades using a high resolution euler solver. Part 1, Formulation and validation [microform] / T.S.R. Reddy ... [et al.].
Text
Washington, DC : National Aeronautics and Space Administration, [1992]
1992
0 resources
Hypersonic vehicle simulation model [microform] : winged-cone configuration / John D. Shaughnessy ... [et al.].
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
1990
0 resources
Modal forced vibration analysis of aerodynamically excited turbosystems [microform] : final report / V. Elchuri.
Text
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1985]
1995
0 resources
Aerodynamics of engine-airframe interaction [microform] : final report / David A. Coughey.
Text
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1988]
1988
0 resources
Prediction of forces and moments for hypersonic flight vehicle control effectors [microform] : progress report and workplan / Mark D. Maughmer.
Text
University Park, PA : Dept. of Aerospace Engineering, Pennsylvania State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1989]
1989
0 resources
A theory for lateral wing-tip blowing [microform] / by D. Tavella and L. Roberts.
Text
[Moffett Field, Calif.] : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1985]
1985
0 resources
Turbine blade-tip clearance excitation forces [microform] : final report on Contract number NAS8-35018 / submitted by M. Martinez-Sanchez and Edward M. Greitzer to NASA, George C. Marshall Space Flight Center, Alabama.
Text
Cambridge, Mass. : Massachusetts Institute of Technology ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1985]
1985
0 resources
Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept [microform] / A.M. Springer.
Text
MSFC, Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Divergence analysis report for the bodies of revolution model support systems [microform] / Larry C. Rash.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1983]
1983
0 resources
SOFIA II model telescope and wind tunnel test [microform] / Paul Keas.
Text
[Moffett Field, Calif.] : NASA Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
ASTROP2 users manual [microform] : a program for aeroelastic stability analysis of propfans / T.S.R. Reddy and John M. Lucero.
Text
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
X-38 vehicle 131 flutter assessment [microform] / James P. Smith.
Text
[Houston, Tex.] : National Aeronautics and Space Administration, Lyndon B. Johnson Space Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
Spatial characteristics of the unsteady differential pressures on 16% F/A-18 vertical tails [microform] : 36th Aerospace Sciences meeting & exhibit : January 12-15, 1998/Reno, NV / Robert W. Moses, Holt Ashley.
Text
Reston, Va. : American Institute of Aeronautics and Astronautics ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
1998
0 resources
On the propagation of small perturbations in two simple aeroelastic systems [microform] / Angelo Iollo, Manuel E. Salas.
Text
Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
1998
0 resources
Estimation of aircraft nonlinear unsteady parameters from wind tunnel data [microform] / Vladislav Klein, Patrick C. Murphy.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
1998
0 resources
Operational data reduction procedure for determining density and vertical structure of the Martian upper atmosphere from Mars global surveyor accelerometer measurements [microform] / George J. Cancro, Robert H. Tolson, and Gerald M. Keating.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
1998
0 resources
Sensitivity analysis for coupled aero-structural systems [microform] / Anthony A. Giunta.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
1999
0 resources
Analysis of aerodynamic coefficients using gust gradient data [microform] : spanwise turbulence effects on airplane response / Erik A. Ringnes and Walter Frost.
Text
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by National Technical Information Service, 1986.
1986
0 resources
Loads and motions of an F-106B flying through thunderstorms [microform] / Roger M. Winebarger.
Text
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1986.
1986
0 resources
XTRAN2L [microform] : a program for solving the general-frequency unsteady transonic small disturbance equation / Woodrow Whitlow, Jr.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1983]
1983
0 resources
A mathematical model of the UH-60 helicopter [microform] / Kathryn B. Hilbert.
Text
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; St. Louis, Mo. : United States Army Aviation Systems Command, [1984]
1984
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS95949A review of shock waves around aeroassisted orbital transfer vehicles / Chul Park.
Text
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1985]
1985
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo8677Free-jet feasibility study of a thermal acoustic shield concept for AST/VCE application : dual stream nozzles : comprehensive data report / B.A. Janardan, J.F. Brausch, and A.O. Price.
Text
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, [1984]
1984
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo4290Free-jet feasibility study of a thermal acoustic shield concept for AST/VCE application [microform] : dual stream nozzles : comprehensive data report / B.A. Janardan, J.F. Brausch, and A.O. Price.
Text
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, [1984]
1984
0 resources
A raster based approach to solar pressure modeling / Theodore W. Wright.
Text
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, June 2014.
2014-6
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo54246ASTROP2 users manual : a program for aeroelastic stability analysis of propfans / T.S.R. Reddy and John M. Lucero.
Text
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, March 1996.
1996-3
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo66479An analytical technique for approximating unsteady aerodynamics in the time domain / H.J. Dunn.
Text
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, November 1980.
1980-11
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo71147Semiempirical method for prediction of aerodynamic forces and moments on a steadily spinning light airplane / Bandu N. Pamadi, Lawrence W. Taylor.
Text
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Division, December 1987.
1987-12
1 resource
Available online
http://purl.fdlp.gov/GPO/gpo76171Development of constraint force equation methodology for application to multi-body dynamics including launch vehicle stage separation / Bandu N. Pamadi [and five others].
Text
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, July 2016.
2016-7
1 resource
Available online
http://purl.fdlp.gov/GPO/gpo76572Estimation of aircraft nonlinear unsteady parameters from wind tunnel data / Vladislav Klein, Patrick C. Murphy.
Text
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, December 1998.
1998-12
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo83868Comparison of Theodorsen's unsteady aerodynamic forces with double lattice generalized aerodynamic forces / Boyd Perry, III.
Text
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, September 2017.
2017-9
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo87607Locally linearized longitudinal and lateral-directional aerodynamic stability and control derivatives for the X-29A aircraft / Gerald D. Budd.
Text
Edwards, California : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, January 1984.
1984-1
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo94316Analysis of aerodynamic coefficients using gust gradient data : spanwise turbulence effects on airplane response / Erik A. Ringnes and Walter Frost.
Text
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, February 1986.
1986-2
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo105577Statistical modeling of space shuttle environmental data : final report / J.D. Tubbs, D.W. Brewer.
Text
Marshall Space Flight Center, Alabama : National Aeronautics and Space Administration, Marshall Space Flight Center, October 1983.
1983-10
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo106618Missile aerodynamics for ascent and re-entry / G.L. Watts, J.W. McCarter.
Text
Huntsville, Alabama : National Aeronautics and Space Administration, Langley Research Center, 2012.
2012
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo37318No results found from Digital Research Books Beta
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