A simplified computer program for the prediction of the linear stability behavior of liquid propellant combustors /

Simplified combustion noise theory yielding a prediction of fluctuating pressure level /

Huff, Ronald G.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

STAR category 71."February 1984"--Cover.Distributed to depository libraries in microfiche.Includes b...

Static stability investigation of a single-stage sounding rocket at Mach numbers from 0.60 to 1.20 /

Ferris, James C.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."June 1967."Includes bibliographical references (p. 8).Mode of access: Internet

Two-dimensional stability of laminar flames /

Mukunda, H. S.
Drummond, J. Philip (John Philip)
Langley Research Center.

January 1992

Prepared at Langley Research Center.Includes bibliographical references (p. 14).Mode of access: Inte...

Technique for predicting high-frequency stability characteristics of gaseous-propellant combustors /

Priem, Richard J.
Yang, Jefferson Y. S. (Jefferson Yuan Sheng), 1939-
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 35).Mode of ac...

A simplified computer program for the prediction of the linear stability behavior of liquid propellant combustors

Mitchell, C. E.
Eckert, K.

August 1979

A program for predicting the linear stability of liquid propellant rocket engines is presented. The ...

Numerical computation of aerodynamic heating of liquid propellants /

Kramer, John L.
Roudebush, William H.
Lowell, Herman H.
Lewis Research Center.

Prepared at Lewis Research Center."April 1960."Cover title.Includes bibliographical references (p. 1...

Program user's manual for optimizing the design of a liquid or gaseous propellant rocket engine with the automated combustor design code AUTOCOM /

Reichel, R. H.
Lewis Research Center.
Aerophysics Research Corporation.

January 1973

"Prepared by Aerophysics Research Corporation ... for Lewis Research Center."Cover title.Includes bi...

Combustion stability of single swirl-can combustor modules using ASTM-A1 liquid fuel /

Niedzwiecki, Richard W.
Jones, Robert E. (Robert Ewing), 1932-
United States. National Aeronautics and Space Administration.
Lewis Research Center.

Combustion stability of single swirl-can combustor modules using ASTM-A1 liquid fuel.Prepared at Lew...

A general method for automatic computation of equilibrium compositions and theoretical rocket performance of propellants /

Gordon, Sanford.
Huff, Vearl N.
Zeleznik, Frank J.
Lewis Research Center.

January 1959

A general computer program for chemical equilibrium and rocket performance calculations was written ...

The development of a three-dimensional partially elliptic flow computer program for combustor research /

Pan, Y. S.
Pittsburgh Energy Research Center.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1978

Nov. 1978.Prepared for Langley Research Center under contract NAS1-15046.Includes bibliographical re...

Computer programs for pressurization (ramp) and pressurized expulsion from a cryogenic liquid propellant tank /

Masters, Philip A.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 81).Mode of ac...

An experimental determination of the dynamic response of a long hydraulic line /

Regetz, John D.
United States. National Aeronautics and Space Administration.

Cover title."December 1960."Fluid mechanics; Propellants; Propulsion system elements; Propulsion sys...

Computer program for calculating the flow field of supersonic ejector nozzles /

Anderson, Bernhard H.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 83).Mode of ac...

Computer program for pulsed thermocouples with corrections for radiation effects /

Will, Herbert A.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

STAR category 61."September 1981--Cover."Lewis Research Center."Includes bibliographical references....

Performance of a low-thrust storable propellant rocket at very low chamber pressure /

Wanhainen, John P.
Ross, Phil S.
DeWitt, Richard L.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Propulsion system elements; Propulsion systems, liquid-fuel rockets; Stab...

Simplified combustion noise theory yielding a prediction of fluctuating pressure level /

Huff, Ronald G.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

STAR category 71."February 1984"--Cover.Distributed to depository libraries in microfiche.Includes b...

Static stability investigation of a single-stage sounding rocket at Mach numbers from 0.60 to 1.20 /

Ferris, James C.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."June 1967."Includes bibliographical references (p. 8).Mode of access: Internet

Two-dimensional stability of laminar flames /

Mukunda, H. S.
Drummond, J. Philip (John Philip)
Langley Research Center.

January 1992

Prepared at Langley Research Center.Includes bibliographical references (p. 14).Mode of access: Inte...

Technique for predicting high-frequency stability characteristics of gaseous-propellant combustors /

Priem, Richard J.
Yang, Jefferson Y. S. (Jefferson Yuan Sheng), 1939-
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 35).Mode of ac...

A simplified computer program for the prediction of the linear stability behavior of liquid propellant combustors

Mitchell, C. E.
Eckert, K.

August 1979

A program for predicting the linear stability of liquid propellant rocket engines is presented. The ...

Numerical computation of aerodynamic heating of liquid propellants /

Kramer, John L.
Roudebush, William H.
Lowell, Herman H.
Lewis Research Center.

Prepared at Lewis Research Center."April 1960."Cover title.Includes bibliographical references (p. 1...

Program user's manual for optimizing the design of a liquid or gaseous propellant rocket engine with the automated combustor design code AUTOCOM /

Reichel, R. H.
Lewis Research Center.
Aerophysics Research Corporation.

January 1973

"Prepared by Aerophysics Research Corporation ... for Lewis Research Center."Cover title.Includes bi...

Combustion stability of single swirl-can combustor modules using ASTM-A1 liquid fuel /

Niedzwiecki, Richard W.
Jones, Robert E. (Robert Ewing), 1932-
United States. National Aeronautics and Space Administration.
Lewis Research Center.

Combustion stability of single swirl-can combustor modules using ASTM-A1 liquid fuel.Prepared at Lew...

A general method for automatic computation of equilibrium compositions and theoretical rocket performance of propellants /

Gordon, Sanford.
Huff, Vearl N.
Zeleznik, Frank J.
Lewis Research Center.

January 1959

A general computer program for chemical equilibrium and rocket performance calculations was written ...

The development of a three-dimensional partially elliptic flow computer program for combustor research /

Pan, Y. S.
Pittsburgh Energy Research Center.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1978

Nov. 1978.Prepared for Langley Research Center under contract NAS1-15046.Includes bibliographical re...

Computer programs for pressurization (ramp) and pressurized expulsion from a cryogenic liquid propellant tank /

Masters, Philip A.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 81).Mode of ac...

An experimental determination of the dynamic response of a long hydraulic line /

Regetz, John D.
United States. National Aeronautics and Space Administration.

Cover title."December 1960."Fluid mechanics; Propellants; Propulsion system elements; Propulsion sys...

Computer program for calculating the flow field of supersonic ejector nozzles /

Anderson, Bernhard H.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 83).Mode of ac...

Computer program for pulsed thermocouples with corrections for radiation effects /

Will, Herbert A.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

STAR category 61."September 1981--Cover."Lewis Research Center."Includes bibliographical references....

Performance of a low-thrust storable propellant rocket at very low chamber pressure /

Wanhainen, John P.
Ross, Phil S.
DeWitt, Richard L.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Propulsion system elements; Propulsion systems, liquid-fuel rockets; Stab...

Simplified combustion noise theory yielding a prediction of fluctuating pressure level /

Huff, Ronald G.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

STAR category 71."February 1984"--Cover.Distributed to depository libraries in microfiche.Includes b...

Static stability investigation of a single-stage sounding rocket at Mach numbers from 0.60 to 1.20 /

Ferris, James C.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."June 1967."Includes bibliographical references (p. 8).Mode of access: Internet

Two-dimensional stability of laminar flames /

Mukunda, H. S.
Drummond, J. Philip (John Philip)
Langley Research Center.

January 1992

Prepared at Langley Research Center.Includes bibliographical references (p. 14).Mode of access: Inte...

A simplified computer program for the prediction of the linear stability behavior of liquid propellant combustors /

Abstract

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A simplified computer program for the prediction of the linear stability behavior of liquid propellant combustors /

Abstract

Extracted data

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