Tables and charts for estimating stall effects on lifting-rotor characteristics /

Force-test investigation of the stability and control characteristics of a 1/8-scale model of a tilt-wing Vertical-Take-Off-and-Landing (VTOL) airplane /

Tosti, Louis P.
Langley Research Center.

January 1960

"NASA TN D-44.""Langley Research Center, Langley Field, Va.""March 1960."Title from cover.Includes b...

An evaluation of linearized vortex theory as applied to single and multiple rotors hovering in and out of ground effect /

Heyson, Harry H.
Langley Research Center.

January 1959

"NASA TN D-43.""Langley Research Center, Langley Field, Va.""September 1959."Title from cover.Includ...

Analysis of acceleration, airspeed and gust-velocity data from a four-engine turboprop transport operating over the eastern United States /

Copp, Martin R.
Fetner, Mary W.
Langley Research Center.

January 1959

"NASA TN D-36.""Langley Research Center, Langley Field, Va.""September 1959."Title from cover.Includ...

Effects of a lower surface jet on the lift-drag ratio of a 45° sweptback wing at a Mach number of 2.01 /

Landrum, Emma Jean.
Langley Research Center.

January 1960

"NASA TN D-183.""Langley Research Center, Langley Field, Va.""March 1960."Title from cover.Includes ...

Experimental investigation of the pressure fluctuations on a flat plate and a cylinder in the slipstream of a hovering rotor /

McKee, John W.
Langley Research Center.

January 1959

"NASA TN D-112.""Langley Research Center, Langley Field, Va.""September 1959."Title from cover.Inclu...

Hovering performance characteristics of a rotor with and without blade-pitch servo-control flaps /

Shivers, James P.
United States. National Aeronautics and Space Administration.

Cover title."January 1967."Includes bibliographical references.Mode of access: Internet

Lift and drag characteristics at subsonic speeds and at a Mach number of 1.9 of a lifting circular cylinder with a fineness ratio of 10 /

Lockwood, Vernard E.
McKinney, Linwood W.
Langley Research Center.

January 1959

"NASA TN D-170.""Langley Research Center, Langley Field, Va.""December 1959."Title from cover.Includ...

Compressibility effects on the hovering performance of a two-blade 10-foot-diameter helicopter rotor operating at tip Mach numbers up to 0.98 /

Jewel, Joesph W.
Langley Research Center.

January 1960

"NASA TN D-245.""Langley Research Center, Langley Field, Va.""April 1960."Cover title.Includes bibli...

The effects of various combinations of damping and control power on helicopter handling qualities during both instrument and visual flight /

Salmirs, Seymour.
Tapscott, Robert J.
Langley Research Center.

January 1959

"NASA TN D-58.""Langley Research Center, Langley Field, Va.""October 1959."Title from cover.Includes...

Experimental investigation at a Mach number of 3.11 of the lift, drag, and pitching-moment characteristics of five blunt lifting bodies /

Letko, William.
Langley Research Center.

January 1960

"NASA TN D-226.""Langley Research Center, Langley Field, Va..""April 1960."Cover title.Includes bibl...

Analysis of helicopter rotor blade torsional oscillations due to stall /

Crimi, Peter, 1935-
U.S. Army Air Mobility Research and Development Laboratory.
Langley Research Center.
Avco Corporation. Systems Division.

January 1975

"Prepared by AVCO Systems Division ... for Langley Research Center."Cover title.Includes bibliograph...

Flight investigation of the effects of an outboard wing-leading-edge modification on stall/spin characteristics of a low-wing, single-engine, T-tail light airplane /

Stough, H. Paul.
Patton, James M., Jr.
DiCarlo, Daniel J.
Langley Research Center.

January 1987

Prepared at Langley Research Center."July 1987"--Cover.Includes bibliographical references (p. 9).Mo...

Flight measurements of the effects of blade out of track on the vibration levels on a tandem rotor helicopter /

United States. National Aeronautics and Space Administration.
Langley Research Center.

"May 1960."Cover title.Includes bibliographical references (p. 13).Mode of access: Internet

Importance of the variation of drag with lift in minimization of satellite entry acceleration /

Grant, Frederick C.
Langley Research Center.

January 1959

"NASA TN D-120.""Langley Research Center, Langley Field, Va.""October 1959."Title from cover.Include...

Full-scale wind-tunnel investigation of the longitudinal characteristics of a tilting-rotor convertiplane /

Koenig, David G.
Kelly, Mark W.
Greif, Richard K.
Ames Research Center.

January 1959

"NASA TN D-35.""Ames Research Center, Moffett Field, Calif.""December 1959."Title from cover.Include...

Force-test investigation of the stability and control characteristics of a 1/8-scale model of a tilt-wing Vertical-Take-Off-and-Landing (VTOL) airplane /

Tosti, Louis P.
Langley Research Center.

January 1960

"NASA TN D-44.""Langley Research Center, Langley Field, Va.""March 1960."Title from cover.Includes b...

An evaluation of linearized vortex theory as applied to single and multiple rotors hovering in and out of ground effect /

Heyson, Harry H.
Langley Research Center.

January 1959

"NASA TN D-43.""Langley Research Center, Langley Field, Va.""September 1959."Title from cover.Includ...

Analysis of acceleration, airspeed and gust-velocity data from a four-engine turboprop transport operating over the eastern United States /

Copp, Martin R.
Fetner, Mary W.
Langley Research Center.

January 1959

"NASA TN D-36.""Langley Research Center, Langley Field, Va.""September 1959."Title from cover.Includ...

Effects of a lower surface jet on the lift-drag ratio of a 45° sweptback wing at a Mach number of 2.01 /

Landrum, Emma Jean.
Langley Research Center.

January 1960

"NASA TN D-183.""Langley Research Center, Langley Field, Va.""March 1960."Title from cover.Includes ...

Experimental investigation of the pressure fluctuations on a flat plate and a cylinder in the slipstream of a hovering rotor /

McKee, John W.
Langley Research Center.

January 1959

"NASA TN D-112.""Langley Research Center, Langley Field, Va.""September 1959."Title from cover.Inclu...

Hovering performance characteristics of a rotor with and without blade-pitch servo-control flaps /

Shivers, James P.
United States. National Aeronautics and Space Administration.

Cover title."January 1967."Includes bibliographical references.Mode of access: Internet

Lift and drag characteristics at subsonic speeds and at a Mach number of 1.9 of a lifting circular cylinder with a fineness ratio of 10 /

Lockwood, Vernard E.
McKinney, Linwood W.
Langley Research Center.

January 1959

"NASA TN D-170.""Langley Research Center, Langley Field, Va.""December 1959."Title from cover.Includ...

Compressibility effects on the hovering performance of a two-blade 10-foot-diameter helicopter rotor operating at tip Mach numbers up to 0.98 /

Jewel, Joesph W.
Langley Research Center.

January 1960

"NASA TN D-245.""Langley Research Center, Langley Field, Va.""April 1960."Cover title.Includes bibli...

The effects of various combinations of damping and control power on helicopter handling qualities during both instrument and visual flight /

Salmirs, Seymour.
Tapscott, Robert J.
Langley Research Center.

January 1959

"NASA TN D-58.""Langley Research Center, Langley Field, Va.""October 1959."Title from cover.Includes...

Experimental investigation at a Mach number of 3.11 of the lift, drag, and pitching-moment characteristics of five blunt lifting bodies /

Letko, William.
Langley Research Center.

January 1960

"NASA TN D-226.""Langley Research Center, Langley Field, Va..""April 1960."Cover title.Includes bibl...

Analysis of helicopter rotor blade torsional oscillations due to stall /

Crimi, Peter, 1935-
U.S. Army Air Mobility Research and Development Laboratory.
Langley Research Center.
Avco Corporation. Systems Division.

January 1975

"Prepared by AVCO Systems Division ... for Langley Research Center."Cover title.Includes bibliograph...

Flight investigation of the effects of an outboard wing-leading-edge modification on stall/spin characteristics of a low-wing, single-engine, T-tail light airplane /

Stough, H. Paul.
Patton, James M., Jr.
DiCarlo, Daniel J.
Langley Research Center.

January 1987

Prepared at Langley Research Center."July 1987"--Cover.Includes bibliographical references (p. 9).Mo...

Flight measurements of the effects of blade out of track on the vibration levels on a tandem rotor helicopter /

United States. National Aeronautics and Space Administration.
Langley Research Center.

"May 1960."Cover title.Includes bibliographical references (p. 13).Mode of access: Internet

Importance of the variation of drag with lift in minimization of satellite entry acceleration /

Grant, Frederick C.
Langley Research Center.

January 1959

"NASA TN D-120.""Langley Research Center, Langley Field, Va.""October 1959."Title from cover.Include...

Full-scale wind-tunnel investigation of the longitudinal characteristics of a tilting-rotor convertiplane /

Koenig, David G.
Kelly, Mark W.
Greif, Richard K.
Ames Research Center.

January 1959

"NASA TN D-35.""Ames Research Center, Moffett Field, Calif.""December 1959."Title from cover.Include...

Force-test investigation of the stability and control characteristics of a 1/8-scale model of a tilt-wing Vertical-Take-Off-and-Landing (VTOL) airplane /

Tosti, Louis P.
Langley Research Center.

January 1960

"NASA TN D-44.""Langley Research Center, Langley Field, Va.""March 1960."Title from cover.Includes b...

An evaluation of linearized vortex theory as applied to single and multiple rotors hovering in and out of ground effect /

Heyson, Harry H.
Langley Research Center.

January 1959

"NASA TN D-43.""Langley Research Center, Langley Field, Va.""September 1959."Title from cover.Includ...

Analysis of acceleration, airspeed and gust-velocity data from a four-engine turboprop transport operating over the eastern United States /

Copp, Martin R.
Fetner, Mary W.
Langley Research Center.

January 1959

"NASA TN D-36.""Langley Research Center, Langley Field, Va.""September 1959."Title from cover.Includ...

Tables and charts for estimating stall effects on lifting-rotor characteristics /

Abstract

Extracted data

Tables and charts for estimating stall effects on lifting-rotor characteristics /

Abstract

Extracted data

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