Modifications to the nozzle test chamber to extend nozzle static-test capability /

Pocketing mechanics of SRM nozzle liner /

Verderaime, V.
George C. Marshall Space Flight Center.

January 1986

Prepared at George C. Marshall Space Flight Center."March 1986"--Cover.Includes bibliographical refe...

Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap /

Re, Richard J.
Leavitt, Laurence D.
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986"--Cover.Includes bibliographical references (p. 15-1...

Operational evaluation of a propeller test stand in the quiet flow facility at Langley Research Center /

Block, P. J. W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

"September 1982"--Cover.Includes bibliographical references.Mode of access: Internet

Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability /

Mason, Mary L.
Burley, James R.
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986"--Cover.Includes bibliographical references (p. 13-1...

Static internal performance of single expansion-ramp nozzles with thrust vectoring and reversing /

Re, Richard J.
Berrier, Bobby L.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

Subject Category 02."March 1982"--Cover."Langley Research Center."Includes bibliographical reference...

Low-speed wind-tunnel tests of an advanced eight-bladed propeller /

Coe, Paul L.
Dunham, Dana Morris.
Gentry, Garl L.
Langley Research Center.

January 1985

Prepared at Langley Research Center."July 1985"--Cover.Includes bibliographical references (p. 4).Mo...

Effect of empennage arrangement on single-engine nozzle/afterbody static pressures at transonic speeds /

Henderson, William P.
Burley, James R.
Langley Research Center.

January 1987

Prepared at Langley Research Center."November 1987"--Cover.Includes bibliographical references (p. 7...

Expanded operational capabilities of the Langley Mach 7 scramjet test facility /

Thomas, Scott R.
Guy, Robert W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1983

"October 1983"--Cover.Distributed to depository libraries in microfiche."Langley Research Center."Mo...

Nozzle wall roughness effects on free-stream noise and transition in the pilot low-disturbance tunnel /

Creel, Theodore R.
Chen, Fang-Jenq.
Beckwith, Ivan E.
Langley Research Center.

January 1985

Prepared at Langley Research Center."September 1985"--Cover.Includes bibliographical references (p. ...

Investigation of a supersonic cruise fighter model flow field /

Reubush, David E.
Bare, E. Ann.
Langley Research Center.

January 1985

Prepared at Langley Research Center."November 1985"--Cover.Includes bibliographical references (p. 8...

Langley mach 4 scramjet test facility /

Andrews, Earl H.
Langley Research Center.

January 1985

Prepared at Langley Research Center."February 1985."Includes bibliographical references (p. 11-12).M...

Static performance of nonaxisymmetric nozzles with yaw thrust-vectoring vanes /

Mason, Mary L.
Berrier, Bobby L.
Langley Research Center.

January 1988

Prepared at Langley Research Center."May 1988"--Cover.Includes bibliographical references (p. 10).Mo...

Static performance of an axisymmetric nozzle with post-exit vanes for multiaxis thrust vectoring /

Berrier, Bobby L.
Langley Research Center.

January 1988

Prepared at Langley Research Center."May 1988"--Cover.Includes bibliographical references (p. 11).Mo...

Experimental thrust performance of a high-area-ratio rocket nozzle /

Pavli, Albert J.
Smith, Tamara A.
Kacynski, Kenneth J.
Lewis Research Center.

January 1987

Prepared at Lewis Research Center."April 1987"--Cover.Includes bibliographical references (p. 13).Mo...

Transition fixing for hypersonic flow /

Sterrett, James R.
Langley Research Center.

Prepared at Langley Research Center."October 1967"--Cover.Includes bibliographical references (p. 12...

Pocketing mechanics of SRM nozzle liner /

Verderaime, V.
George C. Marshall Space Flight Center.

January 1986

Prepared at George C. Marshall Space Flight Center."March 1986"--Cover.Includes bibliographical refe...

Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap /

Re, Richard J.
Leavitt, Laurence D.
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986"--Cover.Includes bibliographical references (p. 15-1...

Operational evaluation of a propeller test stand in the quiet flow facility at Langley Research Center /

Block, P. J. W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

"September 1982"--Cover.Includes bibliographical references.Mode of access: Internet

Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability /

Mason, Mary L.
Burley, James R.
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986"--Cover.Includes bibliographical references (p. 13-1...

Static internal performance of single expansion-ramp nozzles with thrust vectoring and reversing /

Re, Richard J.
Berrier, Bobby L.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

Subject Category 02."March 1982"--Cover."Langley Research Center."Includes bibliographical reference...

Low-speed wind-tunnel tests of an advanced eight-bladed propeller /

Coe, Paul L.
Dunham, Dana Morris.
Gentry, Garl L.
Langley Research Center.

January 1985

Prepared at Langley Research Center."July 1985"--Cover.Includes bibliographical references (p. 4).Mo...

Effect of empennage arrangement on single-engine nozzle/afterbody static pressures at transonic speeds /

Henderson, William P.
Burley, James R.
Langley Research Center.

January 1987

Prepared at Langley Research Center."November 1987"--Cover.Includes bibliographical references (p. 7...

Expanded operational capabilities of the Langley Mach 7 scramjet test facility /

Thomas, Scott R.
Guy, Robert W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1983

"October 1983"--Cover.Distributed to depository libraries in microfiche."Langley Research Center."Mo...

Nozzle wall roughness effects on free-stream noise and transition in the pilot low-disturbance tunnel /

Creel, Theodore R.
Chen, Fang-Jenq.
Beckwith, Ivan E.
Langley Research Center.

January 1985

Prepared at Langley Research Center."September 1985"--Cover.Includes bibliographical references (p. ...

Investigation of a supersonic cruise fighter model flow field /

Reubush, David E.
Bare, E. Ann.
Langley Research Center.

January 1985

Prepared at Langley Research Center."November 1985"--Cover.Includes bibliographical references (p. 8...

Langley mach 4 scramjet test facility /

Andrews, Earl H.
Langley Research Center.

January 1985

Prepared at Langley Research Center."February 1985."Includes bibliographical references (p. 11-12).M...

Static performance of nonaxisymmetric nozzles with yaw thrust-vectoring vanes /

Mason, Mary L.
Berrier, Bobby L.
Langley Research Center.

January 1988

Prepared at Langley Research Center."May 1988"--Cover.Includes bibliographical references (p. 10).Mo...

Static performance of an axisymmetric nozzle with post-exit vanes for multiaxis thrust vectoring /

Berrier, Bobby L.
Langley Research Center.

January 1988

Prepared at Langley Research Center."May 1988"--Cover.Includes bibliographical references (p. 11).Mo...

Experimental thrust performance of a high-area-ratio rocket nozzle /

Pavli, Albert J.
Smith, Tamara A.
Kacynski, Kenneth J.
Lewis Research Center.

January 1987

Prepared at Lewis Research Center."April 1987"--Cover.Includes bibliographical references (p. 13).Mo...

Transition fixing for hypersonic flow /

Sterrett, James R.
Langley Research Center.

Prepared at Langley Research Center."October 1967"--Cover.Includes bibliographical references (p. 12...

Pocketing mechanics of SRM nozzle liner /

Verderaime, V.
George C. Marshall Space Flight Center.

January 1986

Prepared at George C. Marshall Space Flight Center."March 1986"--Cover.Includes bibliographical refe...

Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap /

Re, Richard J.
Leavitt, Laurence D.
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986"--Cover.Includes bibliographical references (p. 15-1...

Operational evaluation of a propeller test stand in the quiet flow facility at Langley Research Center /

Block, P. J. W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

"September 1982"--Cover.Includes bibliographical references.Mode of access: Internet

Modifications to the nozzle test chamber to extend nozzle static-test capability /

Abstract

Extracted data

Modifications to the nozzle test chamber to extend nozzle static-test capability /

Abstract

Extracted data

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