Search Results

1

Minimum weight design of ring and stringer stiffeners for axially compressed cylindrical shells with and without internal pressure /

by Block, David L., 1939-
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1972

Government Document Book

2

A computational examination of directional stability for smooth and chined forebodies at high-[alaph] /

by Ravi, Ramakrishnan
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992

Government Document Book

3

Comparison of wind-tunnel test results at M[subscript infinity] = 0.7 with results from the Boeing TEA-230 subsonic flow method /

by Mohn, Larry Wayne
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1975

Government Document Book

4

An experimental study of the validity of the heat-field concept for sonic-boom alleviation /

by Swigart, Rudolph J.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1974

Government Document Book

5

A fast-acting electrical servo for the actuation of full-span, Fowler-type wing flaps in DLC applications : a detail design study /

by Smetana, Frederick O., 1928-
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1972

Government Document Book

6

Preliminary system design study for a digital fly-by-wire flight control system for an F-8C aircraft /

by Seacord, C. L.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1976

Government Document Book

7

Concepts for manned lunar habitat /

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, 1991

Government Document Book

8

Euler technology assessment program for preliminary aircraft design employing SPLITFLOW code with cartesian unstructured grid method /

by Finley, Dennis B.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, 1995

Government Document Book

9

Some remarks on the design of transonic tunnels with low levels of flow unsteadiness /

by Mabey, Dennis G.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1976

Government Document Book

10

A versatile Mössbauer spectrometer and its applications in vibration measurement /

by Singh, Jag J.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1972

Government Document Book

11

Automated Mars surface sample return mission concepts for achievement of essential scientific objectives /

by Weaver, William L.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1975

Government Document Book

12

Verification of the FtCayuga fault-tolerant microprocessor system /

by Srivas, Mandayam
Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; For sale by the National Technical Information Service, 1991

Government Document Book

13

A simplified approach to axisymmetric dual-reflector antenna design /

by Barger, Raymond L.
Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Division ; For sale by the National Technical Information Service, 1988

Government Document Book

14

Helicopter noise : blade slap /

by Leverton, John W.
Washington, D.C. : National Aeronautics and Space Administration, 1968

Government Document

15

ODIN : Optimal Design Integration System /

by Glatt, C. R.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1975

Government Document Book

16

Numerical method for design of minimum-drag supersonic wing camber with constraints on pitching moment and surface deformation /

by Sorrells, Russell B.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1972

Government Document Book

17

Streamline curvature design procedure for subsonic and transonic ducts /

by Barger, Raymond L.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1973

Government Document Book

18

Guidance, navigation, and control subsystem equipment selection algorithm using expert system methods /

by Allen, Cheryl L.
Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; For sale by the National Technical Information Service, 1991

Government Document Book

19

Design of integrated pitch axis for autopilot/autothrottle and integrated lateral axis for autopilot/yaw damper for NASA TSRV airplane using integral LQG methodology /

Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; For sale by the National Technical Information Service, 1990

Government Document Book

20

Integrated autopilot/autothrottle for the NASA TSRV B-737 aircraft : design and verification by nonlinear simulation /

by Bruce, Kevin R., 1960-
Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Division ; For sale by the National Technical Information Service, 1989

Government Document Book

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