Author Search Results

1

Unsteady blade pressure measurements for the SR-7A propeller at cruise conditions by Heidelberg, Laurence J.

[Washington, DC] : [Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1990

Format: Government Document Book

2

Unsteady blade pressure measurements on a model counterrotation propeller by Heidelberg, Laurence J.

[Washington, DC] : [Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1989

Format: Government Document Book

3

Advanced turboprop wing installation effects measured by unsteady blade pressure and noise by Heidelberg, Laurence J.

[Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1987

Format: Government Document Book

4

Unsteady blade pressure measurements on a model counterrotation propeller by Heidelberg, Laurence J.

[Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1989

Format: Government Document Book

5

Preliminary results of unsteady blade surface pressure measurements for the SR-3 propeller by Heidelberg, Laurence J.

[Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1986

Format: Government Document Book

6

Preliminary results of unsteady blade surface pressure measurements for the SR-3 propeller by Heidelberg, Laurence J.

[Washington, DC] : [Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1986

Format: Government Document Book

7

Acoustic evaluation of the Helmholtz resonator treatment in the NASA Lewis 8- by 6-foot supersonic wind tunnel by Heidelberg, Laurence J.

[Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1989

Format: Government Document Book

8

Advanced turboprop wing installation effects measured by unsteady blade pressure and noise by Heidelberg, Laurence J.

[Washington, D.C.] : [Springfield, Va. : National Aeronautics and Space Administration ; National Technical Information Service, distributor, 1987

Format: Government Document Book

9

Unsteady blade pressure measurements for the SR-7A propeller at cruise conditions by Heidelberg, Laurence J.

[Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1990

Format: Government Document Book

10

Experimental evaluation of a spinning-mode acoustic-treatment design concept for aircraft inlets by Heidelberg, Laurence J.

Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [For sale by the National Technical Information Service], 1980

Format: Government Document Book

11

Acoustic, performance, and wake survey measurements of a lobed velocity-decayer nozzle installed on a quieted TF-34 turbofan engine by Samanich, Nick E.

Washington : Springfield, Va. : U.S. National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1976

Other Authors: “…Heidelberg, Laurence J.…”

Format: Government Document Book

12

Coupling of low speed fan stator vane unsteady pressures to duct modes : measured versus predicted by Sutliff, Daniel L.

[Cleveland, Ohio] : Springfield, VA : National Aeronautics and Space Administration, Glenn Research Center ; National Technical Information Service, distributor, 1999

Other Authors: “…Heidelberg, Laurence J.…”

Format: Government Document Book

13

Acoustic mode measurements in the inlet of a model turbofan using a continuously rotating rake : data collection/analysis techniques by Hall, David G.

[Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [For sale by the National Technical Information Service], 1993

Other Authors: “…Heidelberg, Laurence J.…”

Format: Government Document Book

Unsteady blade pressure measurements for the SR-7A propeller at cruise conditions by Heidelberg, Laurence J.

Unsteady blade pressure measurements on a model counterrotation propeller by Heidelberg, Laurence J.

Advanced turboprop wing installation effects measured by unsteady blade pressure and noise by Heidelberg, Laurence J.

Unsteady blade pressure measurements on a model counterrotation propeller by Heidelberg, Laurence J.

Preliminary results of unsteady blade surface pressure measurements for the SR-3 propeller by Heidelberg, Laurence J.

Preliminary results of unsteady blade surface pressure measurements for the SR-3 propeller by Heidelberg, Laurence J.

Acoustic evaluation of the Helmholtz resonator treatment in the NASA Lewis 8- by 6-foot supersonic wind tunnel by Heidelberg, Laurence J.

Advanced turboprop wing installation effects measured by unsteady blade pressure and noise by Heidelberg, Laurence J.

Unsteady blade pressure measurements for the SR-7A propeller at cruise conditions by Heidelberg, Laurence J.

Experimental evaluation of a spinning-mode acoustic-treatment design concept for aircraft inlets by Heidelberg, Laurence J.

Acoustic, performance, and wake survey measurements of a lobed velocity-decayer nozzle installed on a quieted TF-34 turbofan engine by Samanich, Nick E.

Coupling of low speed fan stator vane unsteady pressures to duct modes : measured versus predicted by Sutliff, Daniel L.

Acoustic mode measurements in the inlet of a model turbofan using a continuously rotating rake : data collection/analysis techniques by Hall, David G.

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