Analysis of wing slipstream flow interaction /

by Jameson, Antony, 1934-, United States. National Aeronautics and Space Administration., Ames Research Center., Grumman Aerospace Corporation.
Published 1970

Ditching investigation of a 1/20-scale model of the space shuttle orbiter /

by Thomas, William L., Langley Research Center., Grumman Aerospace Corporation.
Published 1975

Simulation of hypersonic scramjet exhaust /

by Oman, R. A., Langley Research Center., Grumman Aerospace Corporation.
Published 1975

Thermal dynamic modeling study /

by Ojalvo, I. U., Langley Research Center., Grumman Aerospace Corporation.
Published 1972

Lateral conduction effects on heat-transfer data obtained with the phase-change paint technique /

by Maise, George., Rossi, Michael J., Langley Research Center., Grumman Aerospace Corporation.
Published 1974

Analysis of wing-body interaction flutter for a preliminary space shuttle design /

by Chipman, Richard R., Shyprykevich, Peter., Langley Research Center., Grumman Aerospace Corporation.
Published 1974

Simulation of a hydrocarbon fueled scramjet exhaust /

by Leng, J., United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., Grumman Aerospace Corporation., Langley Research Center.
Published 1982

Development of an apparatus to measure thermophysical properties of wind tunnel heat transfer models /

by Romanowski, Richard F., Steinberg, Ira H., Langley Research Center., Grumman Aerospace Corporation.
Published 1974

Investigation of hydrogen-air ignition senitized by nitric oxide and by nitrogen dioxide /

by Slack, M., Grillo, A., joint author., Grumman Aerospace Corporation., United States. National Aeronautics and Space Administration.
Published 1977

The NCOREL computer program for 3D nonlinear supersonic potential flow computations /

by Siclari, Michael J., United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., Langley Research Center., Grumman Aerospace Corporation.
Published 1983

Study of the use of a phoswich detector for aerial radiometric surveys /

by Schneid, E. J., author., Lagin, L. J., author., National Uranium Resource Evaluation Program., Grumman Aerospace Corporation. Research Department., Bendix Field Engineering Corporation. Grand Junction Operations., United States. Department of Energy. Grand Junction Office.

Control definition study for advanced vehicles /

by Lapins, Maris., Grumman Aerospace Corporation., Langley Research Center., United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Published 1983

A passive flow measurement system for storm and combined sewers /

by Foreman, K. M., United States. Environmental Protection Agency. Office of Research and Development., Grumman Aerospace Corporation.
Published 1976

PLANS : a finite element program for nonlinear analysis of structures.

by Pifko, A., Armen, Harry., Levine, H. S., Langley Research Center., Grumman Aerospace Corporation.
Published 1975

U.S. Coast Guard hybrid concept.

by Meyer, J., Wright, R., Hermanns, E., Grumman Aerospace Corporation. Naval Ship Systems Department., David W. Taylor Naval Ship Research and Development Center., United States. Coast Guard. Office of Research and Development.
Published 1984

A guide for predicting the vibrations of fighter aircraft in the preliminary design stages /

by Ungar, Eric E., author, Air Force Flight Dynamics Laboratory (U.S.), issuing agency., Grumman Aerospace Corporation, sponsor., Bolt, Beranek, and Newman, sponsor.

An algorithm for Liapunov stability analysis of complex nonlinear systems with application to the Orbiting Astronomical Observatory /

by Geiss, Gunther R., Ames Research Center., Grumman Aerospace Corporation.
Published 1971

Tracked air cushion research vehicle subsystems analysis /

by Schlosser, A., United States. Office of High-Speed Ground Transportation., Grumman Aerospace Corporation.
Published [197

Random vibration : decrease corporate cost increase fleet readiness /

by Grumman Aerospace Corporation., United States. Navy Dept. Electronic Systems Command.
Published 1978

A numerically efficient finite element hydroelastic analysis : volume 1--theory and results /

by Coppolino, Robert N., United States. National Aeronautics and Space Administration., Grumman Aerospace Corporation.
Published 1976