Longitudinal stability and control characteristics from a flight investigation of a cruciform canard missile configuration having an exposed wing-canard area ratio of 16:1 /

Lift, drag, and static longitudinal stability data from an exploratory investigation at a Mach number of 6.86 of an airplane configuration having a wing of trapezoidal plan form /

Penland, Jim A.
Fetterman, David E.
Ridyard, Herbert W.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"January 18, 1955."Includes bibliographical references (p. 7).Mode of access: Internet

Stability and control characteristics of a three-surface advanced fighter configuration at angles of attack up to 45?/

Henderson, William P.
Leavitt, Laurence D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"September 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access...

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...

Static longitudinal stability and control characteristics at a mach number of 2.01 of a hypersonic missile configuration having all-movable wing and tail surfaces /

Robinson, Ross B.
Foster, Gerald V.
Langley Research Center.

January 1961

"April 1961."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Stability and control characteristics at Mach numbers from 0.20 to 4.63 of a cruciform air-to-air missile with triangular canard controls and a trapezoidal wing /

Graves, Ernald B.
Fournier, Roger H.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Errata sheet inserted.Chiefly graphs.Cover title.Mode of access:...

Low-speed investigation of effects of vertical tails on the static stability characteristics of a canard-bomber configuration having a very thin wing and a slender elliptical fuselage /

Gainer, Thomas G.
Langley Research Center.

January 1961

"January 1961."Caption title.Includes bibliographical references (p. 8).Mode of access: Internet

Preliminary investigation of the effects of several seeker-nose configurations on the longitudinal characteristics of a canard-type missile at a Mach number of 1.60 /

Robins, A. Warner.

"October 30, 1953. Declassified September 17, 1958"--Cover.Caption title.Includes bibliographical re...

The static and dynamic longitudinal stability characteristics of some supersonic aircraft configurations /

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

January 1952

"January 29, 1952; Declassified July 17, 1958."Includes bibliographical references (p. 10-12).Mode o...

Low-speed static lateral stability characteristics of a canard model having a 60©� triangular wing and horizontal tail /

Bates, William R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1949

"November 23, 1949."Includes bibliographical references (p. 9).Mode of access: Internet

Stability and control characteristics of a monoplanar missile configuration with triform-tail-fin arrangements at mach numbers from 1.70 to 2.86 /

Lamb, Milton.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject Category 02."December 1981"--Cover."Langley Research Center."Bibliography: p. 10.Mode of acc...

Investigation of the dynamic lateral stability and control characteristics of a model of a fighter airplane without a horizontal tail and equipped with either single or twin vertical tails /

Draper, John W.
Rose, Robert W.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1949

"November 15, 1949."Includes bibliographical references (p. 8).Mode of access: Internet

Preliminary results for a free-flight investigation at transonic and supersonic speeds of longitudinal stability and control characteristics of an airplane configuration with a thin straight wing of aspect ratio 3 /

Gillis, Clarence L.
Vitale, A. James.
Peck, Robert F.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1950

"Declassified September 4, 1956.""February 14, 1950."Includes bibliographical references (p. xx).Mod...

Aerodynamic characteristics of a canard-balanced, free-floating, all-movable stabilizer as obtained from rocket-powered-model flight tests and low-speed wind-tunnel tests /

Gardner, William N.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"December 4, 1953."Includes bibliographical references (p. 32-33).Mode of access: Internet

Effect of wing location and strakes on stability and control characteristics of a monoplanar circular missile with low-profile tail fins at supersonic speeds /

Blair, A. B.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Dec. 1980."Langley Research Center."Includes bibliographical references.Mode of access: Internet

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 ...

Lift, drag, and static longitudinal stability data from an exploratory investigation at a Mach number of 6.86 of an airplane configuration having a wing of trapezoidal plan form /

Penland, Jim A.
Fetterman, David E.
Ridyard, Herbert W.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"January 18, 1955."Includes bibliographical references (p. 7).Mode of access: Internet

Stability and control characteristics of a three-surface advanced fighter configuration at angles of attack up to 45?/

Henderson, William P.
Leavitt, Laurence D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"September 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access...

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...

Static longitudinal stability and control characteristics at a mach number of 2.01 of a hypersonic missile configuration having all-movable wing and tail surfaces /

Robinson, Ross B.
Foster, Gerald V.
Langley Research Center.

January 1961

"April 1961."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Stability and control characteristics at Mach numbers from 0.20 to 4.63 of a cruciform air-to-air missile with triangular canard controls and a trapezoidal wing /

Graves, Ernald B.
Fournier, Roger H.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Errata sheet inserted.Chiefly graphs.Cover title.Mode of access:...

Low-speed investigation of effects of vertical tails on the static stability characteristics of a canard-bomber configuration having a very thin wing and a slender elliptical fuselage /

Gainer, Thomas G.
Langley Research Center.

January 1961

"January 1961."Caption title.Includes bibliographical references (p. 8).Mode of access: Internet

Preliminary investigation of the effects of several seeker-nose configurations on the longitudinal characteristics of a canard-type missile at a Mach number of 1.60 /

Robins, A. Warner.

"October 30, 1953. Declassified September 17, 1958"--Cover.Caption title.Includes bibliographical re...

The static and dynamic longitudinal stability characteristics of some supersonic aircraft configurations /

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

January 1952

"January 29, 1952; Declassified July 17, 1958."Includes bibliographical references (p. 10-12).Mode o...

Bates, William R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1949

"November 23, 1949."Includes bibliographical references (p. 9).Mode of access: Internet

Stability and control characteristics of a monoplanar missile configuration with triform-tail-fin arrangements at mach numbers from 1.70 to 2.86 /

Lamb, Milton.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject Category 02."December 1981"--Cover."Langley Research Center."Bibliography: p. 10.Mode of acc...

Investigation of the dynamic lateral stability and control characteristics of a model of a fighter airplane without a horizontal tail and equipped with either single or twin vertical tails /

Draper, John W.
Rose, Robert W.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1949

"November 15, 1949."Includes bibliographical references (p. 8).Mode of access: Internet

Preliminary results for a free-flight investigation at transonic and supersonic speeds of longitudinal stability and control characteristics of an airplane configuration with a thin straight wing of aspect ratio 3 /

Gillis, Clarence L.
Vitale, A. James.
Peck, Robert F.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1950

"Declassified September 4, 1956.""February 14, 1950."Includes bibliographical references (p. xx).Mod...

Aerodynamic characteristics of a canard-balanced, free-floating, all-movable stabilizer as obtained from rocket-powered-model flight tests and low-speed wind-tunnel tests /

Gardner, William N.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"December 4, 1953."Includes bibliographical references (p. 32-33).Mode of access: Internet

Effect of wing location and strakes on stability and control characteristics of a monoplanar circular missile with low-profile tail fins at supersonic speeds /

Blair, A. B.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Dec. 1980."Langley Research Center."Includes bibliographical references.Mode of access: Internet

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 ...

Lift, drag, and static longitudinal stability data from an exploratory investigation at a Mach number of 6.86 of an airplane configuration having a wing of trapezoidal plan form /

Penland, Jim A.
Fetterman, David E.
Ridyard, Herbert W.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"January 18, 1955."Includes bibliographical references (p. 7).Mode of access: Internet

Stability and control characteristics of a three-surface advanced fighter configuration at angles of attack up to 45?/

Henderson, William P.
Leavitt, Laurence D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"September 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access...

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...

Longitudinal stability and control characteristics from a flight investigation of a cruciform canard missile configuration having an exposed wing-canard area ratio of 16:1 /

Abstract

Extracted data

Longitudinal stability and control characteristics from a flight investigation of a cruciform canard missile configuration having an exposed wing-canard area ratio of 16:1 /

Abstract

Extracted data

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