Boundary layer stability on a yawed spinning body of revolution and its effect on the magnus force and moment /

Effect of solidity and inclination on propeller-nacelle force coefficients /

Gentry, Garl L.
Takallu, Mohammad Ali, 1948-
Dunham, Dana Morris.
Langley Research Center.

January 1991

Prepared at Langley Research Center.Includes bibliographical references (p. 6).Mode of access: Inter...

Analysis of stall flutter of a helicopter rotor blade /

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

January 1973

"Prepared by AVCO Systems Division ... for Langley Research Center."Cover title.Bibliography: p. 132...

Effect of support flexibility and damping on the dynamic response of a single mass flexible rotor in elastic bearings /

Kirk, R. Gordon (Robley Gordon)
Gunter, Edgar J.
Lewis Research Center.
University of Virginia.

January 1972

"Prepared by University of Virginia ... for Lewis Research Center."Cover title.Bibliography: p. 35-3...

An experimental investigation of vortex generation in a turbulent boundary layer undergoing adverse pressure gradient /

Zakkay, Victor.
Calarese, Wladimiro.
Langley Research Center.
New York University.

January 1972

"Prepared by New York University ... for Langley Research Center."Cover title.Bibliography: p. 9.Mod...

Flight-measured laminar boundary layer transition phenomena including stability theory analysis /

Obara, Clifford J.
Holmes, Bruce J.
Langley Research Center.

January 1985

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

The effect of acceleration versus displacement methods on steady-state boundary forces /

McGhee, David S.
George C. Marshall Space Flight Center.

January 1992

Prepared at George C. Marshall Space Flight Center.Includes bibliographical references (p. 16).Mode ...

A boundary layer approach to the analysis of atmospheric motion over a surface obstruction /

Frost, Walter, 1935-
Simpson, W. R.
Maus, J. R.
George C. Marshall Space Flight Center.
University of Tennessee (System). Space Institute.

January 1973

"Prepared by the University of Tennessee Space Institute ... for George C. Marshall Space Flight Cen...

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...

Vortex equations : singularities, numerical solution, and axisymmetric vortex breakdown /

Bossel, Hartmut H. (Helmut Hans)
Langley Research Center.
University of California, Santa Barbara.

January 1972

"Prepared by University of California, Santa Barbara ... for Langley Research Center."Cover title.Bi...

An experimental investigation of vortex stability, tip shapes, compressibility, and noise for hovering model rotors /

Tangler, James L.
Miley, Stan J.
Wohlfeld, Robert M.
Langley Research Center.
Bell Helicopter Company.

January 1973

"Prepared by Bell Helicopter Company ... for Langley Research Center."Cover title.Bibliography: p. 7...

Some measurements of the dynamic and static stability of two blunt-nosed, low-fineness-ratio bodies of revolution in free flight at M=4 /

Sort, Barbara J.
Sommer, Simon C.
Ames Research Center.

January 1959

"October 1959."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Turbulent fluid friction of rotating disks /

Cooper, P. (Paul), 1934-
Lewis Research Center.
Case Western Reserve University.

January 1973

"Prepared by Case Western Reserve University ... for Lewis Research Center."Cover title.Bibliography...

Subsonic roll-damping characteristics of a series of wings /

Boyden, Richmond P.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 10-11).Mode ...

Study of stability of large maneuvers of airplanes /

Haddad, Emile K. (Emile Kamel), 1940-
Lockheed-Georgia Company.
Langley Research Center.

January 1974

"August 1974.""Prepared by Lockheed-Georgia Company ... for Langley Research Center."Cover title.Inc...

Stability of the boundary layer;

Chiarulli, Peter, 1921-
Freeman, John Clinton, 1920-

Reproduced from typewritten copy.At head of title: Technical report no. F-TR-1197-1A.Mode of access:...

Effect of solidity and inclination on propeller-nacelle force coefficients /

Gentry, Garl L.
Takallu, Mohammad Ali, 1948-
Dunham, Dana Morris.
Langley Research Center.

January 1991

Prepared at Langley Research Center.Includes bibliographical references (p. 6).Mode of access: Inter...

Analysis of stall flutter of a helicopter rotor blade /

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

January 1973

"Prepared by AVCO Systems Division ... for Langley Research Center."Cover title.Bibliography: p. 132...

Effect of support flexibility and damping on the dynamic response of a single mass flexible rotor in elastic bearings /

Kirk, R. Gordon (Robley Gordon)
Gunter, Edgar J.
Lewis Research Center.
University of Virginia.

January 1972

"Prepared by University of Virginia ... for Lewis Research Center."Cover title.Bibliography: p. 35-3...

An experimental investigation of vortex generation in a turbulent boundary layer undergoing adverse pressure gradient /

Zakkay, Victor.
Calarese, Wladimiro.
Langley Research Center.
New York University.

January 1972

"Prepared by New York University ... for Langley Research Center."Cover title.Bibliography: p. 9.Mod...

Flight-measured laminar boundary layer transition phenomena including stability theory analysis /

Obara, Clifford J.
Holmes, Bruce J.
Langley Research Center.

January 1985

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

The effect of acceleration versus displacement methods on steady-state boundary forces /

McGhee, David S.
George C. Marshall Space Flight Center.

January 1992

Prepared at George C. Marshall Space Flight Center.Includes bibliographical references (p. 16).Mode ...

A boundary layer approach to the analysis of atmospheric motion over a surface obstruction /

Frost, Walter, 1935-
Simpson, W. R.
Maus, J. R.
George C. Marshall Space Flight Center.
University of Tennessee (System). Space Institute.

January 1973

"Prepared by the University of Tennessee Space Institute ... for George C. Marshall Space Flight Cen...

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...

Vortex equations : singularities, numerical solution, and axisymmetric vortex breakdown /

Bossel, Hartmut H. (Helmut Hans)
Langley Research Center.
University of California, Santa Barbara.

January 1972

"Prepared by University of California, Santa Barbara ... for Langley Research Center."Cover title.Bi...

An experimental investigation of vortex stability, tip shapes, compressibility, and noise for hovering model rotors /

Tangler, James L.
Miley, Stan J.
Wohlfeld, Robert M.
Langley Research Center.
Bell Helicopter Company.

January 1973

"Prepared by Bell Helicopter Company ... for Langley Research Center."Cover title.Bibliography: p. 7...

Some measurements of the dynamic and static stability of two blunt-nosed, low-fineness-ratio bodies of revolution in free flight at M=4 /

Sort, Barbara J.
Sommer, Simon C.
Ames Research Center.

January 1959

"October 1959."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Turbulent fluid friction of rotating disks /

Cooper, P. (Paul), 1934-
Lewis Research Center.
Case Western Reserve University.

January 1973

"Prepared by Case Western Reserve University ... for Lewis Research Center."Cover title.Bibliography...

Subsonic roll-damping characteristics of a series of wings /

Boyden, Richmond P.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 10-11).Mode ...

Study of stability of large maneuvers of airplanes /

Haddad, Emile K. (Emile Kamel), 1940-
Lockheed-Georgia Company.
Langley Research Center.

January 1974

"August 1974.""Prepared by Lockheed-Georgia Company ... for Langley Research Center."Cover title.Inc...

Stability of the boundary layer;

Chiarulli, Peter, 1921-
Freeman, John Clinton, 1920-

Reproduced from typewritten copy.At head of title: Technical report no. F-TR-1197-1A.Mode of access:...

Effect of solidity and inclination on propeller-nacelle force coefficients /

Gentry, Garl L.
Takallu, Mohammad Ali, 1948-
Dunham, Dana Morris.
Langley Research Center.

January 1991

Prepared at Langley Research Center.Includes bibliographical references (p. 6).Mode of access: Inter...

Analysis of stall flutter of a helicopter rotor blade /

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

January 1973

"Prepared by AVCO Systems Division ... for Langley Research Center."Cover title.Bibliography: p. 132...

Effect of support flexibility and damping on the dynamic response of a single mass flexible rotor in elastic bearings /

Kirk, R. Gordon (Robley Gordon)
Gunter, Edgar J.
Lewis Research Center.
University of Virginia.

January 1972

"Prepared by University of Virginia ... for Lewis Research Center."Cover title.Bibliography: p. 35-3...

Boundary layer stability on a yawed spinning body of revolution and its effect on the magnus force and moment /

Abstract

Extracted data

Boundary layer stability on a yawed spinning body of revolution and its effect on the magnus force and moment /

Abstract

Extracted data

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