Lateral directional stability characteristics at mach 2.3 to 3.5 of a supersonic transport model with various outboard vertical-tail locations /

Preliminary design study of a lateral-directional control system using thrust vectoring /

Lallman, Frederick J.
Langley Research Center.

January 1985

Prepared at Langley Research Center."November 1985"--Cover.Includes bibliographical references (p. 1...

An analytical study of aircraft lateral-directional handling qualities using pilot models /

Adams, James J.
Moore, Frederick L. (Frederick Lyle), 1943-
Langley Research Center.

January 1976

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 23-24).Mode ...

Subsonic and supersonic longitudinal stability and control characteristics of an aft tail fighter configuration with cambered and uncambered wings and cambered fuselage /

Dollyhigh, Samuel M.
Langley Research Center.

January 1974

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

Experimental and theoretical supersonic lateral-directional stability characteristics of a simplified wing-body configuration with a series of vertical-tail arrangements /

Lamb, Milton.
Thomas, James L. (James Lee), 1952-
Sawyer, Wallace C.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"August 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: I...

Effect of several tail configurations on the stability characteristics of a midwing supersonic-bomber model at mach numbers of 1.60, 1.90, 2.20, and 2.50 /

Wells, R. Franklin.
Silvers, H. Norman.
Langley Research Center.

January 1960

"Langley Research Center, Langley Field, Va.""NASA TM X-279."Cover title.Mode of access: Internet

Longitudinal aerodynamic characteristics at Mach numbers from 0.50 to 1.19 of a supersonic transport model with a modified M wing /

Ray, Edward J.
Taylor, Robert T., NASA researcher.
Langley Research Center.

January 1967

"NASA TM X-1386.""Langley Research Center, Langley Station, Hampton, Va.""June 1967"--Cover.Includes...

Investigation of lateral-directional dynamic stability of a tilt-wing V/STOL transport /

Chambers, Joseph R.
Grafton, Sue B.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1970

Lateral-directional dynamic stability derivatives, characteristics, and handling qualities of tilt-w...

Investigation of the static longitudinal and lateral stability characteristics of a 0.10-scale model of a three-stage configuration of the Scout research vehicle at Mach numbers of 2.29, 2.96, 3.96, and 4.65 /

Jernell, Lloyd S.
Langley Research Center.

Prepared at Langley Research Center."March 1961."Cover title.Includes bibliographical references (p....

Rocket-model investigation of lateral stability characteristics and power effects of a jet-engine airplane configuration with tail boom at mach numbers from 1.15 to 1.37 /

Curry, T. Bradley.
Crabill, Norman L.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Aerodynamics, aircraft; Stability and control.Includes bibliographical re...

High-lift characteristics of a variable-sweep supersonic transport model with a blended engine-fuselage and engine-mounted horizontal tails /

Lockwood, Vernard E.
Langley Research Center.

January 1966

"NASA TM X-1199.""Langley Research Center, Langley Station, Hampton, Va.""March 1966"--Cover.Include...

Miscellaneous directional-stability data for several airplane-like configurations from rocket-model tests at transonic speeds /

Purser, Paul E.
Mitchell, Jesse L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1952

Some approximate values of the yawing moment due to sideslip derivative for eight airplane-like conf...

Effects of vertical-tail size and a ventral fin on the static lateral and directional stability derivatives of a 0.048-scale model of a horizontal-attitude VTOL airplane at transonic speeds /

Olstad, Walter B.
Langley Research Center.

January 1960

"October 1960."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Longitudinal and lateral-directional aerodynamic characteristics of a wing-cone configuration at Mach numbers from 2.5 to 4.5 /

Covell, Peter F.
Howell, Dorothy T.
Walker, Ira J.
Langley Research Center.

January 1992

Prepared at Langley Research Center.Includes bibliographical references (p. 7).Mode of access: Inter...

Static longitudinal, directional, and lateral stability and control data at a mach number of 6.83 of the final configuration of the X-15 research airplane /

Penland, Jim A.
Fetterman, Jr., David E.
Langley Research Center.

January 1960

"April 1960"--Cover.Caption title.Includes bibliographical references (p. 10-11).Mode of access: Int...

Supersonic aerodynamic characteristics of canard, tailless, and aft-tail configurations for two wing planforms /

Covell, Peter F.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 66).M...

Preliminary design study of a lateral-directional control system using thrust vectoring /

Lallman, Frederick J.
Langley Research Center.

January 1985

Prepared at Langley Research Center."November 1985"--Cover.Includes bibliographical references (p. 1...

An analytical study of aircraft lateral-directional handling qualities using pilot models /

Adams, James J.
Moore, Frederick L. (Frederick Lyle), 1943-
Langley Research Center.

January 1976

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 23-24).Mode ...

Subsonic and supersonic longitudinal stability and control characteristics of an aft tail fighter configuration with cambered and uncambered wings and cambered fuselage /

Dollyhigh, Samuel M.
Langley Research Center.

January 1974

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

Experimental and theoretical supersonic lateral-directional stability characteristics of a simplified wing-body configuration with a series of vertical-tail arrangements /

Lamb, Milton.
Thomas, James L. (James Lee), 1952-
Sawyer, Wallace C.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"August 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: I...

Effect of several tail configurations on the stability characteristics of a midwing supersonic-bomber model at mach numbers of 1.60, 1.90, 2.20, and 2.50 /

Wells, R. Franklin.
Silvers, H. Norman.
Langley Research Center.

January 1960

"Langley Research Center, Langley Field, Va.""NASA TM X-279."Cover title.Mode of access: Internet

Longitudinal aerodynamic characteristics at Mach numbers from 0.50 to 1.19 of a supersonic transport model with a modified M wing /

Ray, Edward J.
Taylor, Robert T., NASA researcher.
Langley Research Center.

January 1967

"NASA TM X-1386.""Langley Research Center, Langley Station, Hampton, Va.""June 1967"--Cover.Includes...

Investigation of lateral-directional dynamic stability of a tilt-wing V/STOL transport /

Chambers, Joseph R.
Grafton, Sue B.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1970

Lateral-directional dynamic stability derivatives, characteristics, and handling qualities of tilt-w...

Investigation of the static longitudinal and lateral stability characteristics of a 0.10-scale model of a three-stage configuration of the Scout research vehicle at Mach numbers of 2.29, 2.96, 3.96, and 4.65 /

Jernell, Lloyd S.
Langley Research Center.

Prepared at Langley Research Center."March 1961."Cover title.Includes bibliographical references (p....

Rocket-model investigation of lateral stability characteristics and power effects of a jet-engine airplane configuration with tail boom at mach numbers from 1.15 to 1.37 /

Curry, T. Bradley.
Crabill, Norman L.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Aerodynamics, aircraft; Stability and control.Includes bibliographical re...

High-lift characteristics of a variable-sweep supersonic transport model with a blended engine-fuselage and engine-mounted horizontal tails /

Lockwood, Vernard E.
Langley Research Center.

January 1966

"NASA TM X-1199.""Langley Research Center, Langley Station, Hampton, Va.""March 1966"--Cover.Include...

Miscellaneous directional-stability data for several airplane-like configurations from rocket-model tests at transonic speeds /

Purser, Paul E.
Mitchell, Jesse L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1952

Some approximate values of the yawing moment due to sideslip derivative for eight airplane-like conf...

Effects of vertical-tail size and a ventral fin on the static lateral and directional stability derivatives of a 0.048-scale model of a horizontal-attitude VTOL airplane at transonic speeds /

Olstad, Walter B.
Langley Research Center.

January 1960

"October 1960."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Longitudinal and lateral-directional aerodynamic characteristics of a wing-cone configuration at Mach numbers from 2.5 to 4.5 /

Covell, Peter F.
Howell, Dorothy T.
Walker, Ira J.
Langley Research Center.

January 1992

Prepared at Langley Research Center.Includes bibliographical references (p. 7).Mode of access: Inter...

Static longitudinal, directional, and lateral stability and control data at a mach number of 6.83 of the final configuration of the X-15 research airplane /

Penland, Jim A.
Fetterman, Jr., David E.
Langley Research Center.

January 1960

"April 1960"--Cover.Caption title.Includes bibliographical references (p. 10-11).Mode of access: Int...

Supersonic aerodynamic characteristics of canard, tailless, and aft-tail configurations for two wing planforms /

Covell, Peter F.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 66).M...

Preliminary design study of a lateral-directional control system using thrust vectoring /

Lallman, Frederick J.
Langley Research Center.

January 1985

Prepared at Langley Research Center."November 1985"--Cover.Includes bibliographical references (p. 1...

An analytical study of aircraft lateral-directional handling qualities using pilot models /

Adams, James J.
Moore, Frederick L. (Frederick Lyle), 1943-
Langley Research Center.

January 1976

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 23-24).Mode ...

Subsonic and supersonic longitudinal stability and control characteristics of an aft tail fighter configuration with cambered and uncambered wings and cambered fuselage /

Dollyhigh, Samuel M.
Langley Research Center.

January 1974

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

Lateral directional stability characteristics at mach 2.3 to 3.5 of a supersonic transport model with various outboard vertical-tail locations /

Abstract

Extracted data

Lateral directional stability characteristics at mach 2.3 to 3.5 of a supersonic transport model with various outboard vertical-tail locations /

Abstract

Extracted data

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