The effect of various missile characteristics on airframe frequency response /

Theoretical investigation of effects of changes in command computations and filter location on response of an automatically controlled interceptor during the attack phase /

Sherman, Windsor L.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Missiles and satellite carriers.In...

On frequency measurements and resolution /

Demmerle, Alan M.
Goddard Space Flight Center.

Prepared at Goddard Space Flight Center."December 1964"--Cover.Includes bibliographical references.M...

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

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...

Investigation toward simplification of missile control systems /

Curfman, Howard J.
Crane, Harold L.
Strass, H. Kurt.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1953

"November 12, 1953."Includes bibliographical references (p. 7).Mode of access: Internet

Jet effects at supersonic speeds on base and afterbody pressures of a missile model having single and multiple jets /

Charczenko, Nickolai.
Hayes, Clyde.
Langley Research Center.

Prepared at Langley Research Center."November 1963"--Cover.Includes bibliographical references (p. 8...

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...

Sideslip characteristics at various angles of attack for several hypersonic missile configurations with canard controls at a mach number of 2.01 /

Foster, Gerald V.
Langley Research Center.

January 1959

"November 1959"--Cover.Caption title.Includes bibliographical references (p. 6).Mode of access: Inte...

Landing conditions for large airplanes in routine operations /

Silsby, Norman S.
Harrin, Ezlaslav N.
Langley Aeronautical Laboratory.
United States. National Advisory Committee for Aeronautics.

On front cover: "June 6, 1955; Declassified May 8, 1957."Includes bibliographical references (pages ...

Static investigation of several jet deflectors for longitudinal control of an aircraft /

Valerino, Alfred S.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "June 7, 1955."Title from cover.Includes bibliographical references: p. 9.Mode of ac...

Effect of several airframe/nozzle modifications on the drag of a variable-sweep bomber configuration /

Re, Richard J.
Reubush, David E.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"October 1979"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: ...

The wind-induced loads on a dynamically scaled model of a large missile in launching position /

Buell, Donald A.
Kenyon, George C.
Ames Research Center.

January 1959

"December 1959."Caption title.Includes bibliographical refereneces (p. 13).Mode of access: Internet

Note on performance of aircraft ejector nozzles at high secondary flows /

Kochendorfer, Fred D.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "August 27, 1954."Title from cover.Includes bibliographical references: p. 9.Mode of...

Aerodynamic heating tests of missile stabilizers in a free jet at Mach number 2 /

Vosteen, Louis F.
Langley Research Center.

January 1960

"Declassified February 8, 1963.""September 1960."Cover title.Includes bibliographical references (p....

Water-landing characteristics of a 1/10-scale model of a winged missile /

Fisher, Lloyd J.
United States. National Aeronautics and Space Administration.

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

Theoretical investigation of effects of changes in command computations and filter location on response of an automatically controlled interceptor during the attack phase /

Sherman, Windsor L.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Missiles and satellite carriers.In...

On frequency measurements and resolution /

Demmerle, Alan M.
Goddard Space Flight Center.

Prepared at Goddard Space Flight Center."December 1964"--Cover.Includes bibliographical references.M...

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

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...

Investigation toward simplification of missile control systems /

Curfman, Howard J.
Crane, Harold L.
Strass, H. Kurt.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1953

"November 12, 1953."Includes bibliographical references (p. 7).Mode of access: Internet

Jet effects at supersonic speeds on base and afterbody pressures of a missile model having single and multiple jets /

Charczenko, Nickolai.
Hayes, Clyde.
Langley Research Center.

Prepared at Langley Research Center."November 1963"--Cover.Includes bibliographical references (p. 8...

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...

Sideslip characteristics at various angles of attack for several hypersonic missile configurations with canard controls at a mach number of 2.01 /

Foster, Gerald V.
Langley Research Center.

January 1959

"November 1959"--Cover.Caption title.Includes bibliographical references (p. 6).Mode of access: Inte...

Landing conditions for large airplanes in routine operations /

Silsby, Norman S.
Harrin, Ezlaslav N.
Langley Aeronautical Laboratory.
United States. National Advisory Committee for Aeronautics.

On front cover: "June 6, 1955; Declassified May 8, 1957."Includes bibliographical references (pages ...

Static investigation of several jet deflectors for longitudinal control of an aircraft /

Valerino, Alfred S.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "June 7, 1955."Title from cover.Includes bibliographical references: p. 9.Mode of ac...

Effect of several airframe/nozzle modifications on the drag of a variable-sweep bomber configuration /

Re, Richard J.
Reubush, David E.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"October 1979"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: ...

The wind-induced loads on a dynamically scaled model of a large missile in launching position /

Buell, Donald A.
Kenyon, George C.
Ames Research Center.

January 1959

"December 1959."Caption title.Includes bibliographical refereneces (p. 13).Mode of access: Internet

Note on performance of aircraft ejector nozzles at high secondary flows /

Kochendorfer, Fred D.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "August 27, 1954."Title from cover.Includes bibliographical references: p. 9.Mode of...

Aerodynamic heating tests of missile stabilizers in a free jet at Mach number 2 /

Vosteen, Louis F.
Langley Research Center.

January 1960

"Declassified February 8, 1963.""September 1960."Cover title.Includes bibliographical references (p....

Water-landing characteristics of a 1/10-scale model of a winged missile /

Fisher, Lloyd J.
United States. National Aeronautics and Space Administration.

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

Theoretical investigation of effects of changes in command computations and filter location on response of an automatically controlled interceptor during the attack phase /

Sherman, Windsor L.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Missiles and satellite carriers.In...

On frequency measurements and resolution /

Demmerle, Alan M.
Goddard Space Flight Center.

Prepared at Goddard Space Flight Center."December 1964"--Cover.Includes bibliographical references.M...

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

The effect of various missile characteristics on airframe frequency response /

Abstract

Extracted data

The effect of various missile characteristics on airframe frequency response /

Abstract

Extracted data

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