Theoretical analysis of the rolling motions of aircraft using a flicker-type automatic roll stabilization system having a displacement-plus-rate response /

Analog-computer investigation of effects of friction and preload on the dynamic longitudinal characteristics of a pilot-airplane combination. /

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

January 1957

"November 20, 1957."Includes bibliographical references (p. xx).Mode of access: Internet

Flutter investigation of a true-speed dynamic model with various tip-tank configurations /

Sewall, John L.
Igoe, William B.
Sewall, John L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"March 30, 1955."Stores, airplane components; Vibration and flutter; wings and ailerons.Includes bib...

Flight measurement of the stability characteristics of the Douglas D-558-1 airplane (Buaero no. 37971) in sideslips /

Williams, Walter C.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1949

"April 18, 1949."Includes bibliographical references (p. 5).Mode of access: Internet

Preliminary investigation at low speeds of swept wings in rolling flow /

Feigenbaum, David.
Goodman, Alex.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1947

"May 22, 1947."Includes bibliographical references (p. 12).Mode of access: Internet

An analysis of the effects of aeroelasticity on static longitudinal stability and control of a swept-back-wing airplane /

Skoog, Richard B.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "August 27, 1951."Includes bibliographical references: p. 29.Mode of access: Interne...

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

Several factors affecting roll control systems of interceptors /

Sternfield, Leonard.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"November 6, 1953."Includes bibliographical references (p. 7).Mode of access: Internet

Experimental and analytical investigation of flutter of a nonuniform sweptback cantilever wing with two concentrated weights /

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

January 1951

"December 4, 1951."Includes bibliographical references (p. 17).Mode of access: Internet

Experimental determination of effect of structural rigidity on rolling effectiveness of some straight and swept wings at Mach numbers from 0.7 to 1.7 /

Strass, H. Kurt.
Purser, Paul E.
Fields, E. M.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1950

"October 4, 1950."Includes bibliographical references (p. 11).Mode of access: Internet

The influence of response feedback loops on the lateral-directional dynamics of a variable-stability transport aircraft /

Szalai, Kenneth J.
Flight Research Center (U.S.)
United States. National Aeronautics and Space Administration.

January 1967

Cover title."May 1967."Includes bibliographical references (p. 45).Mode of access: Internet

Experimental determination of the effects of frequency and amplitude of oscillation on the roll-stability derivatives for a 60©� delta-wing airplane model /

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

January 1958

"February 24, 1958."Includes bibliographical references (p. 16).Mode of access: Internet

Flutter characteristics of swept wings at transonic speeds /

Loftin, Laurence K.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"July 6, 1955."Includes bibliographical references (p. 10).Mode of access: Internet

An analysis of the normal accelerations and airspeeds of several Lockheed Constellation L-649 airplanes in postwar commercial transport operations over the eastern part of the United States /

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

January 1950

"April 11, 1950."Includes bibliographical references (p. 9).Mode of access: Internet

Summary of flutter experiences as a guide to the preliminary design of lifting surfaces on missiles /

Martin, Dennis J.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1951

"November 9, 1951."Includes bibliographical references (p. 12).Mode of access: Internet

Investigation of wing flutter at transonic speeds for six systematically varied wing plan forms /

Jones, George W.
DuBose, Hugh C.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"August 13, 1953."Includes bibliographical references (p. 15).Mode of access: Internet

Analog-computer investigation of effects of friction and preload on the dynamic longitudinal characteristics of a pilot-airplane combination. /

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

January 1957

"November 20, 1957."Includes bibliographical references (p. xx).Mode of access: Internet

Flutter investigation of a true-speed dynamic model with various tip-tank configurations /

Sewall, John L.
Igoe, William B.
Sewall, John L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"March 30, 1955."Stores, airplane components; Vibration and flutter; wings and ailerons.Includes bib...

Flight measurement of the stability characteristics of the Douglas D-558-1 airplane (Buaero no. 37971) in sideslips /

Williams, Walter C.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1949

"April 18, 1949."Includes bibliographical references (p. 5).Mode of access: Internet

Preliminary investigation at low speeds of swept wings in rolling flow /

Feigenbaum, David.
Goodman, Alex.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1947

"May 22, 1947."Includes bibliographical references (p. 12).Mode of access: Internet

An analysis of the effects of aeroelasticity on static longitudinal stability and control of a swept-back-wing airplane /

Skoog, Richard B.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "August 27, 1951."Includes bibliographical references: p. 29.Mode of access: Interne...

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

Several factors affecting roll control systems of interceptors /

Sternfield, Leonard.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"November 6, 1953."Includes bibliographical references (p. 7).Mode of access: Internet

Experimental and analytical investigation of flutter of a nonuniform sweptback cantilever wing with two concentrated weights /

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

January 1951

"December 4, 1951."Includes bibliographical references (p. 17).Mode of access: Internet

Experimental determination of effect of structural rigidity on rolling effectiveness of some straight and swept wings at Mach numbers from 0.7 to 1.7 /

Strass, H. Kurt.
Purser, Paul E.
Fields, E. M.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1950

"October 4, 1950."Includes bibliographical references (p. 11).Mode of access: Internet

The influence of response feedback loops on the lateral-directional dynamics of a variable-stability transport aircraft /

Szalai, Kenneth J.
Flight Research Center (U.S.)
United States. National Aeronautics and Space Administration.

January 1967

Cover title."May 1967."Includes bibliographical references (p. 45).Mode of access: Internet

Experimental determination of the effects of frequency and amplitude of oscillation on the roll-stability derivatives for a 60©� delta-wing airplane model /

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

January 1958

"February 24, 1958."Includes bibliographical references (p. 16).Mode of access: Internet

Flutter characteristics of swept wings at transonic speeds /

Loftin, Laurence K.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"July 6, 1955."Includes bibliographical references (p. 10).Mode of access: Internet

An analysis of the normal accelerations and airspeeds of several Lockheed Constellation L-649 airplanes in postwar commercial transport operations over the eastern part of the United States /

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

January 1950

"April 11, 1950."Includes bibliographical references (p. 9).Mode of access: Internet

Summary of flutter experiences as a guide to the preliminary design of lifting surfaces on missiles /

Martin, Dennis J.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1951

"November 9, 1951."Includes bibliographical references (p. 12).Mode of access: Internet

Investigation of wing flutter at transonic speeds for six systematically varied wing plan forms /

Jones, George W.
DuBose, Hugh C.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"August 13, 1953."Includes bibliographical references (p. 15).Mode of access: Internet

Analog-computer investigation of effects of friction and preload on the dynamic longitudinal characteristics of a pilot-airplane combination. /

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

January 1957

"November 20, 1957."Includes bibliographical references (p. xx).Mode of access: Internet

Flutter investigation of a true-speed dynamic model with various tip-tank configurations /

Sewall, John L.
Igoe, William B.
Sewall, John L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"March 30, 1955."Stores, airplane components; Vibration and flutter; wings and ailerons.Includes bib...

Flight measurement of the stability characteristics of the Douglas D-558-1 airplane (Buaero no. 37971) in sideslips /

Williams, Walter C.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1949

"April 18, 1949."Includes bibliographical references (p. 5).Mode of access: Internet

Theoretical analysis of the rolling motions of aircraft using a flicker-type automatic roll stabilization system having a displacement-plus-rate response /

Abstract

Extracted data

Theoretical analysis of the rolling motions of aircraft using a flicker-type automatic roll stabilization system having a displacement-plus-rate response /

Abstract

Extracted data

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