Books on the topic 'Aircraft application'

J, Glassman Arthur, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program, eds. Turbine design and application. Washington, DC: Scientific and Technical Information Program, National Aeronautics and Space Administration, 1994.

Noor, Ahmed Khairy. Advances in contact algorithms and their application to tires. Hampton, Va: Langley Research Center, 1988.

H, Mayrand C., and Lewis Research Center, eds. Multiple-purpose subsonic naval aircraft (MPSNA): Multiple application propfan study (MAPS). Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1986.

H, Mayrand C., and Lewis Research Center, eds. Multiple-purpose subsonic naval aircraft (MPSNA): Multiple application propfan study (MAPS). Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1986.

Julian, Wolkovitch, and Ames Research Center, eds. Application of the joined wing to tiltrotor aircraft. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.

Maine, Richard E. Application of parameter estimation to highly unstable aircraft. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1986.

Sanjay, Garg, Merrill Walter C, and United States. National Aeronautics and Space Administration., eds. Neural network application to aircraft control system design. [Washington, DC]: National Aeronautics and Space Administration, 1991.

Vincent, James H. Application of modern control design methodology to oblique wing research aircraft. Palo Alto, Calif: Systems Control Technology, Inc., 1991.

Nguyen, Hung Lee. Application of mixing-controlled combustion models to gas turbine combustors. [Washington, DC]: National Aeronautics and Space Administration, 1990.

Nguyen, Hung Lee. Application of mixing-controlled combustion models to gas turbine combustors. [Washington, DC]: National Aeronautics and Space Administration, 1990.

Greaney, John. Evaluation of intergrated graphical displays for aircraft cockpit application. Birmingham: University of Birmingham, 1994.

Hinds, H. A. Second quarterly report on the application of modified stepwise regression for the estimation of aircraft stability and control parameters. Cranfield, Bedford, England: Cranfield Institute of Technology, College of Aeronautics, 1989.

S, Narayanaswamy, and United States. National Aeronautics and Space Administration., eds. Integrator windup protection: Techniques and a STOVL aircraft engine controller application : final report. [Washington, DC: National Aeronautics and Space Administration, 1997.

Lv, Peijian. Power-Based Study of Boundary Layer Ingestion for Aircraft Application. Singapore: Springer Nature Singapore, 2023. http://dx.doi.org/10.1007/978-981-19-5497-9.

National Research Council (U.S.). National Materials and Manufacturing Board, ed. Application of lightweighting technology to military aircraft, vessels, and vehicles. Washington, D.C: National Academies Press, 2012.

Klein, Vladislav. Two biased estimation techniques in linear regression: Application to aircraft. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.

Hyde, Richard Alden. H ∞%x; Aerospace Control Design: A VSTOL Flight Application. London: Springer London, 1995.

Hinds, H. A. Third quarterly report on the application of modified stepwise regression for the estimation of aircraft stability and control parameters. Cranfield, Bedford: College of Aeronautics, Cranfield Institute of Technology, 1989.

Cook, M. V. Initial review of research into the application of modified stepwise regression for the estimation of aircraft stability and control parameters. Cranfield, Bedford: College of Aeronautics, Cranfield Institute of Technology, 1989.

Krishna, Kundu, Ghorashi Bahman, and United States. National Aeronautics and Space Administration., eds. Simplified Jet-A kinetic mechanism for combustor application. [Washington, DC: National Aeronautics and Space Administration, 1993.

P, Kundu Krishna, Ghorashi Bahman, and United States. National Aeronautics and Space Administration., eds. Simplified Jet-A kinetic mechanism for combustor application. [Washington, DC: National Aeronautics and Space Administration, 1993.

P, Kundu Krishna, Ghorashi Bahman, and United States. National Aeronautics and Space Administration., eds. Simplified Jet-A kinetic mechanism for combustor application. [Washington, DC: National Aeronautics and Space Administration, 1993.

Field, Edmund. The application of a C* flight control law to large civil transport aircraft. Cranfield, Bedford, England: Cranfield Institute of Technology, College of Aeronautics, 1993.

Steinke, W. E. Analysis of the USDA Forest Service 1988 Aircraft Spray Characterization Trials. Davis, Calif: USDA Forest Service Forest Pest Management, 1992.

M, Engelbeck R., and Lewis Research Center, eds. Multiple-purpose subsonic naval aircraft (MPSNA): Multiple application propfan study (MAPS). Cleveland, Ohio: National Aeronautics and Space Administration , Lewis Research Center, 1988.

Optimization based clearance of flight control laws: A civil aircraft application. Berlin: Springer, 2012.

Hyde, R. A. H [infinity] aerospace control design: A VSTOL flight application. Berlin: Springer, 1995.

Mineck, Raymond E. Application of two procedures for dual-point design of transonic airfoils. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

Mineck, Raymond E. Application of two procedures for dual-point design of transonic airfoils. Hampton: National Aeronautics and Space Administration, Langley Research Center, 1994.

Mineck, Raymond E. Application of two procedures for dual-point design of transonic airfoils. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

Kim, Kyun O. Computational methods for frictionless contact with application to space shuttle orbiter nose-gear tires. Hampton, Va: Langley Research Center, 1991.

Ng, Poh H. Application of triggered lightning numerical models to the F106B and extension to other aircraft. Hampton, Va: Langley Research Center, 1988.

1870-1952, Tillema H. F., MacGregor G. R, and Langley Research Center, eds. Application of analysis techniques for low frequency interior noise and vibration of commercial aircraft. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

Curbishley, Thomas B. 1991 CASPR spray aircraft efficiency model: Validation study. Davis, CA: USDA Forest Service, Forest Pest Management, 1992.

R, Larson Richard, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. A knowledge based application of the extended aircraft interrogation and display system. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

Center, Langley Research, ed. Application of hybrid laminar flow control to global range military transport aircraft. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.

Denis J. S. R. Bertrand. Application of neural network to adaptive control theory for super-augmented aircraft. Monterey, Calif: Naval Postgraduate School, 1991.

Hinton, David A. A candidate wake vortex strength definition for application to the NASA Aircraft Vortex Spacing System (AVOSS). Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

United States. National Aeronautics and Space Administration., ed. Performance analysis of two early NACA high speed propellers with application to civil tiltrotor configurations. [Washington, DC]: National Aeronautics and Space Administration, 1996.

Bilanin, Alan J. Interaction of spray aircraft wake with convective surface winds in hilly terrain. Davis, CA: USDA Forest Service, 1996.

Facility, Dryden Flight Research, ed. Real-time application of advanced three-dimensional graphic techniques for research aircraft simulation. Edwards, Calif: NASA Ames Research Center, Dryden Flight Research Facility, 1990.

G, Farris Glenn, Vanags Andrejs A, and Ames Research Center, eds. A head up display for application to V/STOL aircraft approach and landing. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.

Merrick, Vernon K. A head up display for application to V/STOL aircraft approach and landing. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.

W, Iliff Kenneth, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Application of parameter estimation to aircraft stability and control: The output-error approach. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

Model-based failure-modes-and-effects analysis and its application to aircraft subsystems. Heidelberg: AKA. Verlag, 2009.

Facility, Dryden Flight Research, ed. Real-time application of advanced three-dimensional graphic techniques for research aircraft simulation. Edwards, Calif: NASA Ames Research Center, Dryden Flight Research Facility, 1990.

W, Iliff Kenneth, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Application of parameter estimation to aircraft stability and control: The output-error approach. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

Maine, Richard E. Application of parameter estimation to aircraft stability and control: The output-error approach. Washington, D.C: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

Facility, Dryden Flight Research, ed. Real-time application of advanced three-dimensional graphic techniques for research aircraft simulation. Edwards, Calif: NASA Ames Research Center, Dryden Flight Research Facility, 1990.

Singh, Amit Kumar. Analysis and Design of Power Converter Topologies for Application in Future More Electric Aircraft. Singapore: Springer Singapore, 2018. http://dx.doi.org/10.1007/978-981-10-8213-9.