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Books on the topic 'Flight characteristics'

Author: Grafiati
Published: 4 June 2021
Last updated: 26 July 2025

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1

Rego, Ashley Titus. Simulating the response characteristics of flight instruments. Dept. of Aerospace Science and Engineering, 1985.

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2

Christodoulidis, Theoharis. Robustness characteristics of active flight control algorithms. University of Salford, 1987.

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3

Center, Ames Research, ed. Parametric study of supersonic STOVL flight characteristics. NASA Ames Research Center, 1985.

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4

Development, North Atlantic Treaty Organization Advisory Group for Aerospace Research and. Space vehicle flight mechanics. AGARD, 1990.

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5

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Space vehicle flight mechanics. AGARD, 1990.

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6

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Space vehicle flight mechanics. AGARD, 1990.

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7

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Advances in flying qualities. AGARD, 1988.

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8

Air Force Human Resources Laboratory., ed. Display characteristics of example light-valve projectors. Air Force Human Resources Laboratory, Air Force Systems Command, 1989.

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9

J, Burken John, Maine Trindel A, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Flight testing a propulsion-controlled aircraft emergency flight control system on an F-15 airplane. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1994.

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10

Grant, Peter Robert. Motion characteristics of the UTIAS Flight Research Simulator Motion-base. Dept. of Aerospace Science and Engineering, 1985.

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11

Grant, Peter Robert. Motion characteristics of the UTIAS Flight Research Simulator motion-base. Institute for Aerospace Studies, 1986.

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12

Sim, Alex G. Flight characteristics of a modified Schweizer SGS 1-36 sailplane at low and very high angles of attack. Ames Research Center, 1990.

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13

Johnson, D. E. Investigation of interactions between limb-manipulator dynamics and effective vehicle roll control characteristics. Ames Research Center, 1986.

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14

Stinton, Darrol. Flying qualities and flight testing of the aeroplane. Blackwell Science, 1996.

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15

Stinton, Darrol. Flying qualities and flight testing of the aeroplane. Blakwell Science, 1996.

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16

Ray, J. K. High-speed civil transport flight- and propulsion-control technological issues. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1992.

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17

Ray, J. K. High-speed civil transport flight- and propulsion-control technological issues. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1992.

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18

B, Davidson John, Schmidt D. K, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. A simulation study of the flight dynamics of elastic aircraft. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1987.

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19

Coe, Paul L. Low-speed wind-tunnel investigation of the flight dynamic characteristics of an advanced turboprop business/commuter aircraft configuration. Langley Research Center, 1990.

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20

E, Curry Robert, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Flight characteristics of the AD-1 oblique-wing research aircraft. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

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21

United States. National Aeronautics and Space Administration., ed. Measurement of human pilot dynamic characteristics in flight simulation: Thesis ... National Aeronautics and Space Administration, 1987.

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22

Padfield, G. D. Helicopter flight dynamics: The theory and applicationof flying qualities and simulation modelling. Blackwell Science, 1996.

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23

United States. National Aeronautics and Space Administration. and Dryden Flight Research Facility, eds. Engine exhaust characteristics evaluation in support of aircraft acoustic testing. National Aeronautics and Space Administration, 1993.

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24

Schroeder, Jeffery Allyn. Helicopter flight simulation motion platform requirements. National Aeronautics and Space Administration, Ames Research Center, 1999.

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25

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Comparison of flying qualities derived from in-flight and ground-based simulators for a jet-transport airplane for the approach and landing pilot tasks. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

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26

Foss, Van Zante Judith, and Lewis Research Center, eds. In-flight aerodynamic measurements of an iced horizontal tailplane. National Aeronautics and Space Administration, Lewis Research Center, 1999.

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27

Foss, Van Zante Judith, and Lewis Research Center, eds. In-flight aerodynamic measurements of an iced horizontal tailplane. National Aeronautics and Space Administration, Lewis Research Center, 1999.

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28

Foss, Van Zante Judith, and Lewis Research Center, eds. In-flight aerodynamic measurements of an iced horizontal tailplane. National Aeronautics and Space Administration, Lewis Research Center, 1999.

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29

Padfield, G. D. Helicopter flight dynamics: The theory and application of flying qualities and simulation modelling. 2nd ed. Blackwell, 2007.

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30

Padfield, G. D. Helicopter flight dynamics: The theory and application of flying qualities and simulation modelling. 2nd ed. American Institute of Aeronautics and Astronautics, 2007.

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31

Stinton, Darrol. Flying qualities and flight testing of the airplane. Blackwell Science, 1998.

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32

Stinton, Darrol. Flying qualities and flight testing of the airplane. American Institute of Aeronautics and Astronautics, 1998.

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33

Center, Langley Research, ed. Data mining of NASA Boeing 737 flight data: Frequency analysis of in-flight recorded data. National Aeronautics and Space Administration, Langley Research Center, 2001.

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34

Center, Langley Research, ed. Data mining of NASA Boeing 737 flight data: Frequency analysis of in-flight recorded data. National Aeronautics and Space Administration, Langley Research Center, 2001.

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35

Maine, Richard E. Identification of dynamic systems - applications to aircraft. AGARD, 1986.

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36

Facility, Dryden Flight Research, ed. Initial flight test of a ground deployed system for flying qualities assessment. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1989.

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37

Gibson, J. C. Development of a methodology for excellence in handling qualities design for fly by wire aircraft. Delft University Press, 1999.

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38

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Structures and Materials Panel. Working Group 27. Structures and Materials Panel Working Group 27 on evaluation of loads from operational flight maneuvers: Final Working Group report (L'évaluation des charges résultant des manoeuvres en vol.). AGARD, 1996.

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39

Facility, Dryden Flight Research, ed. Modeling, simulation, and flight characteristics of an aircraft designed to fly at 100,000 feet. National Aeronautics and Space Administration, Dryden Flight Research Facility, 1991.

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40

Vladislav, Klein, and United States. National Aeronautics and Space Administration., eds. Accuracy of aerodynamic model parameters estimated from flight test data. American Institute of Aeronautics and Astronautics, 1997.

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41

G, Turner Steven, Owens D. B. 1922-, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Low-speed wind-tunnel investigation of the flight flight dynamic characteristics of an advanced turboprop business/computer aircraft configuraion. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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42

G, Turner Steven, Owens D. B. 1922-, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Low-speed wind-tunnel investigation of the flight flight dynamic characteristics of an advanced turboprop business/computer aircraft configuraion. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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43

Micol, John R. Hypersonic lateral and directional stability characteristics of Aeroassist Flight Experiment configuration in air and CF4. Langley Research Center, 1993.

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44

Volodko, A. M. Osnovy letnoĭ ėkspluatat͡s︡ii vertoletov: Dinamika poleta. "Transport", 1986.

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45

Dante, Jackson, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Supersonic flying qualities experience using the SR-71. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

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46

R, Phillips Michael, Person Lee H, and Langley Research Center, eds. Investigation of piloting aids for manual control of hypersonic maneuvers. National Aeronautics and Space Administration, Langley Research Center, 1995.

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47

McRuer, Duane T. Assessment of flying-quality criteria for air-breathing aerospacecraft. NASA, 1992.

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48

Center, Ames Research, ed. Influence of lift offset on rotorcraft performance. National Aeronautics and Space Administration, Ames Research Center, 2009.

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49

D, Grantham William, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Ground-based and in-flight simulator studies of flight characteristics of a twin-fuselage passenger transport airplane during approach and landing. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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50

D, Grantham William, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Ground-based and in-flight simulator studies of flight characteristics of a twin-fuselage passenger transport airplane during approach and landing. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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