Chemical nonequilibrium effects on the inviscid flow in the windward plane of symmetry of two simplified shuttle configurations /

Parametric trade studies on a Shuttle II launch system architecture /

Stanley, Douglas O. (Douglas Oliver)
Langley Research Center.

January 1991

Prepared at Langley Research Center.Bibliography: p. 47.Mode of access: Internet

Analytical and experimental vibration studies of a 1/8 scale shuttle orbiter /

Pinson, Larry D.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 69-71).Mode ...

Study of physiological and behavioral response to transitions between rotating and nonrotating environments /

Brady, James F.
Langley Research Center.
General Dynamics Corporation. Convair Division.

January 1972

"Prepared by General Dynamics, Convair Aerospace Division ... for Langley Research Center."Cover ti...

Effects of vibrational nonequilibrium on the inviscid design of an axisymmetric nozzle for hypersonic flow /

Anders, John Benjamin.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 20-22).Mode ...

The effect of finite thrust and heating constraints on the synergetic plane change maneuver for a space shuttle orbiter-class vehicle /

Dickmanns, Ernst Dieter.
George C. Marshall Space Flight Center.

January 1973

Prepared at George C. Marshall Space Flight Center.Cover title.Bibliography: p. 37-38.Mode of access...

Investigation of nonlinear inviscid and viscous flow effects in the analysis of dynamic stall /

Crimi, Peter, 1935-
Langley Research Center.
Avco Corporation. Systems Division.

January 1974

"Prepared by AVCO Systems Division ... for Langley Research Center."Cover title.Bibliography: p. 111...

Upper-stage space-shuttle propulsion by means of separate scramjet and rocket engines /

Franciscus, Leo C.
Allen, John L.
Lewis Research Center.

January 1972

Prepared at Lewis Research Center.Cover title.Bibliography: p. 46-48.Mode of access: Internet

Aeroacoustic and aerodynamic applications of the theory of nonequilibrium thermodynamics /

Horne, W. Clifton (William Clifton)
Karamcheti, Krishnamurty.
Smith, Charles A. (Charles Arthur), 1945-
Ames Research Center.

January 1991

Prepared at Ames Research Center.Bibliography: p. 20-21.Mode of access: Internet

Influence of configuration details on the subsonic characteristics of a space shuttle orbiter design /

Decker, John P.
Phillips, W. Pelham.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 9).Mode of a...

Wind-tunnel roll-damping measurements of a winged space shuttle configuration in launch attitude /

Hess, R. W. (Robert W.)
Davenport, Edwin E.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 9).Mode of a...

Crossflow in two-dimensional asymmetric nozzles /

Sebacher, Daniel I.
Lee, Louis P.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 10).Mode of ...

Hypersonic aerodynamics and entry-maneuver--aerothermodynamic interactions for two lifting entry vehicles /

Arrington, James P.
Woods, William C.
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 12.Mode of access: Internet

Effects of chemical dissociation and molecular vibrations on steady one-dimensional flow /

Heims, Steve P. (Steve Paul)
Ames Research Center.

Prepared at Ames Research Center."August 1959."Cover title.Includes bibliographical references (p. 4...

Jet effects on the drag of conical afterbodies at spersonic speeds /

Compton, William B.
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 13.Mode of access: Internet

Effect of Reynolds number and engine nacelles on the stalling characteristics of a model of a twin-engine light airplane /

Lockwood, Vernard E.
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 9.Mode of access: Internet

Parametric trade studies on a Shuttle II launch system architecture /

Stanley, Douglas O. (Douglas Oliver)
Langley Research Center.

January 1991

Prepared at Langley Research Center.Bibliography: p. 47.Mode of access: Internet

Analytical and experimental vibration studies of a 1/8 scale shuttle orbiter /

Pinson, Larry D.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 69-71).Mode ...

Study of physiological and behavioral response to transitions between rotating and nonrotating environments /

Brady, James F.
Langley Research Center.
General Dynamics Corporation. Convair Division.

January 1972

"Prepared by General Dynamics, Convair Aerospace Division ... for Langley Research Center."Cover ti...

Effects of vibrational nonequilibrium on the inviscid design of an axisymmetric nozzle for hypersonic flow /

Anders, John Benjamin.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 20-22).Mode ...

The effect of finite thrust and heating constraints on the synergetic plane change maneuver for a space shuttle orbiter-class vehicle /

Dickmanns, Ernst Dieter.
George C. Marshall Space Flight Center.

January 1973

Prepared at George C. Marshall Space Flight Center.Cover title.Bibliography: p. 37-38.Mode of access...

Investigation of nonlinear inviscid and viscous flow effects in the analysis of dynamic stall /

Crimi, Peter, 1935-
Langley Research Center.
Avco Corporation. Systems Division.

January 1974

"Prepared by AVCO Systems Division ... for Langley Research Center."Cover title.Bibliography: p. 111...

Upper-stage space-shuttle propulsion by means of separate scramjet and rocket engines /

Franciscus, Leo C.
Allen, John L.
Lewis Research Center.

January 1972

Prepared at Lewis Research Center.Cover title.Bibliography: p. 46-48.Mode of access: Internet

Aeroacoustic and aerodynamic applications of the theory of nonequilibrium thermodynamics /

Horne, W. Clifton (William Clifton)
Karamcheti, Krishnamurty.
Smith, Charles A. (Charles Arthur), 1945-
Ames Research Center.

January 1991

Prepared at Ames Research Center.Bibliography: p. 20-21.Mode of access: Internet

Influence of configuration details on the subsonic characteristics of a space shuttle orbiter design /

Decker, John P.
Phillips, W. Pelham.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 9).Mode of a...

Wind-tunnel roll-damping measurements of a winged space shuttle configuration in launch attitude /

Hess, R. W. (Robert W.)
Davenport, Edwin E.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 9).Mode of a...

Crossflow in two-dimensional asymmetric nozzles /

Sebacher, Daniel I.
Lee, Louis P.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 10).Mode of ...

Hypersonic aerodynamics and entry-maneuver--aerothermodynamic interactions for two lifting entry vehicles /

Arrington, James P.
Woods, William C.
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 12.Mode of access: Internet

Effects of chemical dissociation and molecular vibrations on steady one-dimensional flow /

Heims, Steve P. (Steve Paul)
Ames Research Center.

Prepared at Ames Research Center."August 1959."Cover title.Includes bibliographical references (p. 4...

Jet effects on the drag of conical afterbodies at spersonic speeds /

Compton, William B.
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 13.Mode of access: Internet

Effect of Reynolds number and engine nacelles on the stalling characteristics of a model of a twin-engine light airplane /

Lockwood, Vernard E.
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 9.Mode of access: Internet

Parametric trade studies on a Shuttle II launch system architecture /

Stanley, Douglas O. (Douglas Oliver)
Langley Research Center.

January 1991

Prepared at Langley Research Center.Bibliography: p. 47.Mode of access: Internet

Analytical and experimental vibration studies of a 1/8 scale shuttle orbiter /

Pinson, Larry D.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 69-71).Mode ...

Study of physiological and behavioral response to transitions between rotating and nonrotating environments /

Brady, James F.
Langley Research Center.
General Dynamics Corporation. Convair Division.

January 1972

"Prepared by General Dynamics, Convair Aerospace Division ... for Langley Research Center."Cover ti...

Chemical nonequilibrium effects on the inviscid flow in the windward plane of symmetry of two simplified shuttle configurations /

Abstract

Extracted data

Chemical nonequilibrium effects on the inviscid flow in the windward plane of symmetry of two simplified shuttle configurations /

Abstract

Extracted data

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