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21.
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NASA Technical Note [NASA TN D-450]: Noise considerations for manned reentry vehicles
by Washington. National Aeronautics and Space Administration (NASA) | Hilton, David A | Mayes, William H | Hubbard, Harvey H. Material type:  Book Description: 13p.Publisher: Washington NASA 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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22.
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NASA TN [D-5053]
: TENSILE BEHAVIOR OF BORON-FILAMENT-REINFORCED EPOXY RINGS AND BELTS
by Baucom, Robert M. Description: 29p.Publisher: NASA, Washington, D.C. 1969Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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23.
|
Effects of a retronozzle located at the apex of a 140 deg blunt cone at Mach numbers of 3.00, 4.50, and 6.00 [NASA TN D-6002]
by Mcghee, Robert J. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 38p.Publisher: Washington, D. C. NASA 1971Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-6002] (1).
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24.
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HYPERSONIC FLUTTER ANALYSIS USING MEASURED STATIC AERODYNAMIC DERIVATIVES, AND COMPARISON WITH EXPERIMENT [NASA TN D-5233]
by Goetz, Robert C. Material type: Book Description: 51p.Publisher: Washington, D.C. Naational Aeronautics and Space Administration 1969Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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25.
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OPTICAL PROBING OF SUPERSONIC AERODYNAMIC TURBULENCE WITH STATISTICAL CORRELATION PHASE I
: FEASIBILITY
by Funk, B. H | Cikanek, H. A | Marshall, George C. Material type: Book; Format:
print
; Literary form:
not fiction
Description: xiv, 130p.Publisher: Washington, D.C. Nasa 1971Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-6077] (1).
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26.
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A THEOTETICAL STUDY OF THE EFFECT OF PIVOT LOCATION ON THE AERODYNAMIC-CENTER MOVEMENTS OF VARIABLE-SWEEP WINGS IN INCOMPRESSIBLE FLOW [NASA TN D-4635]
by Lamar,John E. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 28p.Publisher: Washington, D.C. National Aeronautics and Space Administration 1968Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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27.
|
NASA Memorandum [NASA MEMO 4-27-59A]: Lift-drag ratios for an arrow wing with bodies at mach number 3
by Washington. National Aeronautics and Space Administration (NASA) | Jorgensen, Leland H. Material type: Book Description: 32p.Publisher: Washington NASA 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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28.
|
Aerodynamic design and analysis system for supersonic aircraft. [NASA CR-2520] [Bound With NASA CR-2515-2518,2521, Lack No. 2519]
by Middleton, W. D | Lundry, J. L. Material type: Book; Format:
print
; Literary form:
not fiction
Description: various pagings.Publisher: Washington, D.C. NASA 1975Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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29.
|
Aerodynamic design and analysis system for supersonic aircraft [NASA CR-2521] [Bound With NASA CR-2515-2520,Lack No. 2519]
: part ii user manual
by Middleton, W. D | Lundry, J. L | Coleman, R. G. Material type: Book; Format:
print
; Literary form:
not fiction
Description: various pagings.Publisher: Washington, D.C. NASA. 1975Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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30.
|
NASA TN [D-5671]
: SIMULATION OF THE FOKKER-PLANCK EQUATION BY RANDOM WALKS OF TEST PARTICLES IN VELOCITY SPACE WITH APPLICATION TO MAGNETIC MIRROR SYSTEMS
by Englert,Gerald W. Description: 75p.Publisher: Washington D.C. National Aeronautics and Space Administration 1970Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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31.
|
Transonic investigation of aerodynamic characteristics of a swept-wing fighter-airplane model with leading -edge droop in combination with outboard chord-extensions and notches [NASA TN D-834]
by Whitcomb, Charles F | Norton, Harry T. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 30p.Publisher: Washington, D.C. Nasa 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-834] (1).
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32.
|
Aerodynamic characteristics over a mach number range of 1.40 to 2.78 of a rocket -propelled airplane configuration having a low 52.5 (degree) delta wing and an unswept horizontal tail [NASA TN D-836]
by Kehlet, Alan B. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 26p.Publisher: Washington, D.C. Nasa 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-836] (1).
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33.
|
Aerodynamic characteristics in ground effect of a large-scale model with a high disk-loading lifting fan mounted in the fuselage [NASA TN D-1557]
by Desavigny, Richard A | Hickey, David H. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 51p.Publisher: Washington, D.C. Nasa 1963Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-1557] (1).
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34.
|
NASA Technical Note [NASA TN D-5045]: Tuft-grid surveys at low speeds for delta wings
by Washington. National Aeronautics and Space Administration (NASA) | Bird, John D. Material type: Book Description: 31p.Publisher: Washington NASA 1969Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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35.
|
NASA Technical Note [NASA TN D-5044]: Fortran program for calculating velocities and streamlines on a blade-to-blade stream surface of a tandem blade turbomachine
by Washington. National Aeronautics and Space Administration (NASA) | Katsanis, Theodore | McNally, William D. Material type: Book Description: 109p.Publisher: Washington NASA 1969Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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36.
|
NASA Technical Note [NASA TN D-5047]: Full-scale investigation of the aerodynamic characteristics of a sailwing of aspect ratio 5.9
by Washington. National Aeronautics and Space Administration (NASA) | Fink, Marvin P. Material type: Book Description: 30p.Publisher: Washington NASA 1969Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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37.
|
Aerodynamic intraction effects ahead of a sonic jet exhausting perpendiculary from a flat plate in to a mach number 6 free stream
by Romeo, David J | Sterrett, James R. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 26p.Publisher: Washington D. C. NASA 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-743] (1).
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38.
|
Downwash tables for the calculation of aerodynamic forces on oscillating wings
by | National Physical Laboratory. Material type: Book Description: iv, 174p.Publisher: New Delhi National Physical Laboratory 1958Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NPLA RM-2956/1958] (1).
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39.
|
Aerodynamic capture of particles
by | Richardson, E. G., Ed. Material type: Book Description: viii, 200p.Publisher: Oxford Pergamon Press 1960Availability: Items available for loan: PK Kelkar Library, IIT Kanpur [Call number: 531.36 B777a] (1).
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40.
|
High temperature effects in aircraft structures
by | Hoff, Nicholas John [Ed.] | Advisory group for aeronautical research and development North Atlantic treaty organization. Material type: Book Description: vii, 357p.Publisher: London Pergamon 1958Availability: Items available for loan: PK Kelkar Library, IIT Kanpur [Call number: 629.505 Ad9ag] (1).
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