Książki na temat „Aerodynamic loads”

Development, North Atlantic Treaty Organization Advisory Group for Aerospace Research and. Aircraft dynamic loads due to flow separation. Neuilly sur Seine, France: AGARD, 1990.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Aircraft dynamic loads due to flow separation. Neuilly-sur-Seine: AGARD, 1990.

Dillenius, Marnix F. E. Improvements to the missile aerodynamic prediction code DEMON3. Hampton, Va: Langley Research Center, 1992.

Winebarger, Roger M. Loads and motions of an F-106B flying through thunderstorms. Washington, D.C: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

L, Peterson Randall, i Ames Research Center, red. Full-scale hingeless rotor performance and loads. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1995.

L, Peterson Randall, i Ames Research Center, red. Full-scale hingeless rotor performance and loads. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1995.

L, Peterson Randall, i Ames Research Center, red. Full-scale hingeless rotor performance and loads. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1995.

Baumann, Peter Helmut. Messung von aerodynamisch bedingten Modellverformungen im Windkanal mittels Moire-Interferometrie. Koln, Germany: DLR, 1994.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Aircraft loads due to turbulence and their impact on design and certification. Neuilly sur Seine, France: AGARD, 1994.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Aircraft loads due to turbulence and their impact on design and certification. Neuilly sur Seine, France: AGARD, 1994.

Kerr, Patricia A. User's guide: Steady-state aerodynamic-loads program for shuttle TPS tiles. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1986.

Lee, B. H. K. Forced oscillation of a two-dimensional airfoil with nonlinear aerodynamic loads. Ottawa: National Aeronautical Establishment, 1986.

Kerr, Patricia A. User's guide: Steady-state aerodynamic-loads program for shuttle TPS tiles. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1986.

Badavi, Forooz F. Numerical simulation and comparison of symmetrical/supercritical airfoils for the near tip region of a helicopter in forward flight. Hampton, Va: Langley Research Center, 1989.

Houbolt, John C. Manual on the flight of flexible aircraft in turbulence. Neuilly sur Seine, France: Advisory Group for Aerospace Research & Development, 1991.

G, Bousman William, i Ames Research Center, red. Aerodynamic limitations of the UH-60A rotor. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1996.

McMaster, Hal C. FAR 23 loads: Computer aided engineering for airplane loads to federal air regulations. [Wichita, Kan.] (7415 Tanglewood Ct., Wichita 67206): Aero Science Software, 1991.

C, Hall Kenneth, i United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., red. Development of a linearized unsteady aerodynamic analysis for cascade gust response predictions. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

Waldman, W. An improved computational procedure for the unsteady doublet lattice method. Melbourne, Australia: Aeronautical Research Laboratories, 1986.

Martin, Colin A. Surface pressure measurements on the wing of a wind tunnel model during steady rotation. Melbourne, Australia: Aeronautical Research Laboratory, 1991.

Emre, Ilgin Hüseyin, red. Tall buildings: Structural systems and aerodynamic form. London: Routledge, Taylor & Francis Group, 2014.

Center, Langley Research, red. Implementation of a trailing-edge flap analysis model in the NASA Langley CAMRAD.MOD1/HIRES program. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

Center, Langley Research, red. Implementation of a trailing-edge flap analysis model in the NASA Langley CAMRAD.MOD1/HIRES program. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

R, Quackenbush Todd, i Ames Research Center, red. Computation of rotor aerodynamic loads in forward flight using a full-span free wake analysis. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.

R, Quackenbush Todd, i Ames Research Center, red. Computation of rotor aerodynamic loads in forward flight using a full-span free wake analysis. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.

V, Sankewitsch, i Langley Research Center, red. Calculation of flight vibration levels of the AH-1G helicopter and correlation with existing flight vibration measurements. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.

Michel, Gaubert, i Ames Research Center, red. Structural and aerodynamic loads and performance measurements of SA349/2 helicopter with an advanced geometry rotor. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.

Center, Ames Research, i American Helicopter Society, red. Rotorcraft dynamics 1984: Proceedings of the 2nd decennial Specialists' Meeting on Rotorcraft Dynamics sponsored by NASA Ames Research Center and the American Helicopter Society and held at NASA Ames Research Center, Moffett Field, California, November 7-9, 1984. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1985.

United States. National Aeronautics and Space Administration., red. System dynamic analysis of a wind tunnel model with applications to improve aerodynamic data quality: A dissertation ... [Washington, D.C: National Aeronautics and Space Administration, 1997.

Jimmy, Fung, i Langley Research Center, red. Parameter estimation of actuators for Benchmark Active Control Technology (BACT) wind tunnel model with analysis of wear and aerodynamic loading effects. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

Walter, Frost, i United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., red. Analysis of aerodynamic coefficients using gust gradient data: Spanwise turbulence effects on airplane response. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

L, Luz P., i George C. Marshall Space Flight Center., red. Preliminary in-flight loads analysis of in-line launch vehicles using the VLOADS 1.4 program. [Marshall Space Flight Center], Ala: National Aeronautics and Space Administration, Marshall Space Flight Center, 1998.

L, Luz P., i George C. Marshall Space Flight Center., red. Preliminary in-flight loads analysis of in-line launch vehicles using the VLOADS 1.4 program. [Marshall Space Flight Center], Ala: National Aeronautics and Space Administration, Marshall Space Flight Center, 1998.

L, Luz P., i George C. Marshall Space Flight Center., red. Preliminary in-flight loads analysis of in-line launch vehicles using the VLOADS 1.4 program. [Marshall Space Flight Center], Ala: National Aeronautics and Space Administration, Marshall Space Flight Center, 1998.

R, Pamidi P., i Lewis Research Center, red. NASTRAN supplemental documentation for modal forced vibration analysis of aerodynamically excited turbosystems: Final report. Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1985.

R, Ellis John. Specimen designs for testing advanced aeropropulsion materials under in-plane biaxial loading. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2003.

United States. National Aeronautics and Space Administration., red. A CFD/CSD interaction methodology for aircraft wings: A dissertation ... [Washington, DC: National Aeronautics and Space Administration, 1997.

United States. National Aeronautics and Space Administration., red. A numerical model of unsteady, subsonic aeroelastic behavior. [Washington, D.C: National Aeronautics and Space Administration, 1987.

S, Dhadwal Harbans, i NASA Glenn Research Center, red. Simultaneous optical measurements of axial and tangential steady-state blade deflections. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

S, Dhadwal Harbans, i NASA Glenn Research Center, red. Simultaneous optical measurements of axial and tangential steady-state blade deflections. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

Pramote, Dechaumphai, Thornton Earl A. 1936- i Langley Research Center, red. Finite element thermo-viscoplastic analysis of aerospace structures. Hampton, Va: NASA Langley Research Center, 1990.

Pandey, Ajay K. Finite element thermo-viscoplastic analysis of aerospace structures. Hampton, Va: NASA Langley Research Center, 1990.

Pramote, Dechaumphai, Thornton Earl A. 1936- i Langley Research Center, red. Finite element thermo-viscoplastic analysis of aerospace structures. Hampton, Va: NASA Langley Research Center, 1990.

Pramote, Dechaumphai, Thornton Earl A. 1936- i Langley Research Center, red. Finite element thermo-viscoplastic analysis of aerospace structures. Hampton, Va: NASA Langley Research Center, 1990.

United States. National Aeronautics and Space Administration. Office of the Chief Engineer. Evaluation of the NASA arc jet capabilities to support mission requirements. Washington, D.C.]: National Aeronautics and Space Administration, Office of the Chief Engineer, 2010.

Center, Langley Research, red. Inviscid flow computations of the orbital sciences X-34 over a Mach number range of 1.25 to 6.0. Hampton, Va: National Aeronautics and Science Administration, Langley Research Center, 2001.

Kiyoshi, Aoyagi, i Ames Research Center, red. Time-averaged aerodynamic loads on the vane sets of the 40- by 80-foot and 80- by 120-foot wind tunnel complex. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.

Hamade, Karen S. Modal analysis of UH-60A instrumented rotor blades. Moffett Field, Calif: Ames Research Center, 1990.

Hamade, Karen S. Modal analysis of UH-60A instrumented rotor blades. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

M, Kufeld Robert, Ames Research Center i United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., red. Modal analysis of UH-60A instrumented rotor blades. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.