Missile aerodynamic parameter and structure identification from flight test data /

Aerodynamic characteristics of a Sparrow III missile model in the flow field of a generalized parent body at Mach 2.86 /

Stallings, Robert L.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1981

"February 1984"--Cover.Includes bibliographical references.Mode of access: Internet

Prediction of forces and moments on finned missiles at high angle of attack in transonic flow /

Oberkampf, William L., 1944-., author.
United States. Air Force. Systems Command. sponsor.
Air Force Armament Laboratory. issuing body.

"Program Element 61102F-JON 2307E103.""Final Report for period October 1978-September 1979.""October...

Flight investigation of the zero-lift drag of two ram-jet missile configurations at Mach numbers from 1.0 to 1.89 /

Brown, Clarence A.
Bressette, Walter E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"March 9, 1953."Includes bibliographical references (p. 10).Mode of access: Internet

Missile supersonic/hypersonic aerodynamics /

Jenn, Andrew A., author.
Wang, Philip K., author.
Matthews, Carol D., author.
McDonnell Douglas Astronautics Company-St. Louis.
Air Force Flight Dynamics Laboratory (U.S.), sponsor.
Wright Laboratory (Wright-Patterson Air Force Base, Ohio), sponsor.
United States. Air Force. Systems Command, issuing body.

"Final Report for Period September 1989 - May 1991.""May 1991."Includes bibliographical references (...

Wind tunnel tests of a full-scale air-launched cruise missile with an installed turbofan engine /

McDill, H. E., author.
United States. Air Force. Systems Command. issuing body.
Arnold Engineering Development Center, sponsor.
ARO, Inc., sponsor.

Photocopy."February 1977.""Final Report: December 1975 - July 1976."Includes bibliographical referen...

Aerodynamic test and analysis of a slender generic missile configuration /

Gates, Roger S., author
Fische, Mark A., author.
Cipolla, John R., author.
Winchenback, G. L., author.
United States. Air Force. Systems Command. sponsor.
Air Force Armament Laboratory. issuing body.

"Program Element No. 62602F, Project No. 2567, Task No, 03, Work Unit Accession No. 12.""Interim Rep...

Missile Supersonic/Hypersonic Aerodynamics (MSHA) : QUADSTREAM User's/Reference manual /

Deters, Keneth J., author.
Wright Laboratory (Wright-Patterson Air Force Base, Ohio), issuing body.
McDonnell Douglas Astronautics Company-St. Louis, sponsor.

"Final report for period: September 1991 - May 1992.""May 1992."Research supported by the United Sta...

Aerodynamics of supersonic lifting bodies /

Jischke, M. C. (Martin C.). author.
Rasmussen, M. L., author.
United States. Air Force. Systems Command. sponsor.
Air Force Armament Laboratory. issuing body.
University of Oklahoma. School of Aerospace, Mechanical, and Nuclear Engineering. sponsor.

"PE: 61102F, JON: 2307E105.""Final Report October 1977 to September 1980.""February 1981."Includes b...

The effect of various missile characteristics on airframe frequency response /

Matthews, Howard F.
McNeill, Walter E., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "January 7, 1952, Declassified December 13, 1957."Includes bibliographical reference...

A method for obtaining aerodynamic coefficients from yawsonde and radar data /

Whyte, Robert H.
Mermagen, W. H.
U.S. Army Ballistic Research Laboratory.
U.S. Atomic Energy Commission.

"March 1973."Includes bibliographical references (page 29).RDT&E Project No. :Mode of access: Intern...

Analysis and compilation of missile aerodynamic data.

Nichols, James O.
Auburn University. Dept. of Aerospace Engineering.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1977

This summary document was prepared in order to facilitate dissemination of a large amount of missile...

Missile Datcom : User's manual -- rev 4/91 /

Bruns, Kevin D., author.
Vukelich, Steven R., author.
Stoy, Stan L., author.
Moore, Marvin E., author.
Wright Laboratory (Wright-Patterson Air Force Base, Ohio), issuing body.
McDonnell Douglas Astronautics Company-St. Louis, sponsor.

"Final Report for Period May 1987 - April 1991.""April 1991."Includes bibliographical references (pa...

Lateral aerodynamic parameters extracted from light data for the F-8C airplane in maneuvering flight /

Suit, William T. (William Tull), 1937-
United States. National Aeronautics and Space Administration.

January 1977

Issued Mar. 1977.Includes bibliographical references (p. 15).Mode of access: Internet

A Compilation of static stability and fin loads data for slender body missile models with and without tail fins and wings.

Gomillion, G. R., author.
ARO, Inc. sponsor.
Air Force Armament Laboratory (U.S.). sponsor.
United States. Air Force. Arnold Air Force Base. sponsor.
United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body.

"AFATL-TR-76-23.""Prepared for Air Force Armament Laboratory (AFATL/DLMA) Eglin Air Force Base, Flor...

Analysis and compilation of missile aerodynamic data /

Burkhalter, John E.
Auburn University. Dept. of Aerospace Engineering.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1977

This report provides a general analysis of the flight dynamics of several surface-to-air and two air...

Aerodynamic characteristics of a Sparrow III missile model in the flow field of a generalized parent body at Mach 2.86 /

Stallings, Robert L.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1981

"February 1984"--Cover.Includes bibliographical references.Mode of access: Internet

Prediction of forces and moments on finned missiles at high angle of attack in transonic flow /

Oberkampf, William L., 1944-., author.
United States. Air Force. Systems Command. sponsor.
Air Force Armament Laboratory. issuing body.

"Program Element 61102F-JON 2307E103.""Final Report for period October 1978-September 1979.""October...

Flight investigation of the zero-lift drag of two ram-jet missile configurations at Mach numbers from 1.0 to 1.89 /

Brown, Clarence A.
Bressette, Walter E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"March 9, 1953."Includes bibliographical references (p. 10).Mode of access: Internet

Missile supersonic/hypersonic aerodynamics /

Jenn, Andrew A., author.
Wang, Philip K., author.
Matthews, Carol D., author.
McDonnell Douglas Astronautics Company-St. Louis.
Air Force Flight Dynamics Laboratory (U.S.), sponsor.
Wright Laboratory (Wright-Patterson Air Force Base, Ohio), sponsor.
United States. Air Force. Systems Command, issuing body.

"Final Report for Period September 1989 - May 1991.""May 1991."Includes bibliographical references (...

Wind tunnel tests of a full-scale air-launched cruise missile with an installed turbofan engine /

McDill, H. E., author.
United States. Air Force. Systems Command. issuing body.
Arnold Engineering Development Center, sponsor.
ARO, Inc., sponsor.

Photocopy."February 1977.""Final Report: December 1975 - July 1976."Includes bibliographical referen...

Aerodynamic test and analysis of a slender generic missile configuration /

Gates, Roger S., author
Fische, Mark A., author.
Cipolla, John R., author.
Winchenback, G. L., author.
United States. Air Force. Systems Command. sponsor.
Air Force Armament Laboratory. issuing body.

"Program Element No. 62602F, Project No. 2567, Task No, 03, Work Unit Accession No. 12.""Interim Rep...

Missile Supersonic/Hypersonic Aerodynamics (MSHA) : QUADSTREAM User's/Reference manual /

Deters, Keneth J., author.
Wright Laboratory (Wright-Patterson Air Force Base, Ohio), issuing body.
McDonnell Douglas Astronautics Company-St. Louis, sponsor.

"Final report for period: September 1991 - May 1992.""May 1992."Research supported by the United Sta...

Aerodynamics of supersonic lifting bodies /

Jischke, M. C. (Martin C.). author.
Rasmussen, M. L., author.
United States. Air Force. Systems Command. sponsor.
Air Force Armament Laboratory. issuing body.
University of Oklahoma. School of Aerospace, Mechanical, and Nuclear Engineering. sponsor.

"PE: 61102F, JON: 2307E105.""Final Report October 1977 to September 1980.""February 1981."Includes b...

The effect of various missile characteristics on airframe frequency response /

Matthews, Howard F.
McNeill, Walter E., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "January 7, 1952, Declassified December 13, 1957."Includes bibliographical reference...

A method for obtaining aerodynamic coefficients from yawsonde and radar data /

Whyte, Robert H.
Mermagen, W. H.
U.S. Army Ballistic Research Laboratory.
U.S. Atomic Energy Commission.

"March 1973."Includes bibliographical references (page 29).RDT&E Project No. :Mode of access: Intern...

Analysis and compilation of missile aerodynamic data.

Nichols, James O.
Auburn University. Dept. of Aerospace Engineering.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1977

This summary document was prepared in order to facilitate dissemination of a large amount of missile...

Missile Datcom : User's manual -- rev 4/91 /

Bruns, Kevin D., author.
Vukelich, Steven R., author.
Stoy, Stan L., author.
Moore, Marvin E., author.
Wright Laboratory (Wright-Patterson Air Force Base, Ohio), issuing body.
McDonnell Douglas Astronautics Company-St. Louis, sponsor.

"Final Report for Period May 1987 - April 1991.""April 1991."Includes bibliographical references (pa...

Lateral aerodynamic parameters extracted from light data for the F-8C airplane in maneuvering flight /

Suit, William T. (William Tull), 1937-
United States. National Aeronautics and Space Administration.

January 1977

Issued Mar. 1977.Includes bibliographical references (p. 15).Mode of access: Internet

A Compilation of static stability and fin loads data for slender body missile models with and without tail fins and wings.

Gomillion, G. R., author.
ARO, Inc. sponsor.
Air Force Armament Laboratory (U.S.). sponsor.
United States. Air Force. Arnold Air Force Base. sponsor.
United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body.

"AFATL-TR-76-23.""Prepared for Air Force Armament Laboratory (AFATL/DLMA) Eglin Air Force Base, Flor...

Analysis and compilation of missile aerodynamic data /

Burkhalter, John E.
Auburn University. Dept. of Aerospace Engineering.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1977

This report provides a general analysis of the flight dynamics of several surface-to-air and two air...

Aerodynamic characteristics of a Sparrow III missile model in the flow field of a generalized parent body at Mach 2.86 /

Stallings, Robert L.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1981

"February 1984"--Cover.Includes bibliographical references.Mode of access: Internet

Prediction of forces and moments on finned missiles at high angle of attack in transonic flow /

Oberkampf, William L., 1944-., author.
United States. Air Force. Systems Command. sponsor.
Air Force Armament Laboratory. issuing body.

"Program Element 61102F-JON 2307E103.""Final Report for period October 1978-September 1979.""October...

Flight investigation of the zero-lift drag of two ram-jet missile configurations at Mach numbers from 1.0 to 1.89 /

Brown, Clarence A.
Bressette, Walter E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"March 9, 1953."Includes bibliographical references (p. 10).Mode of access: Internet

Missile aerodynamic parameter and structure identification from flight test data /

Abstract

Extracted data

Missile aerodynamic parameter and structure identification from flight test data /

Abstract

Extracted data

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